From b8cebbd335feb321a6c1011b620a92c47de1c3b2 Mon Sep 17 00:00:00 2001 From: sylvain-guillet Date: Sat, 27 May 2023 14:57:26 +0200 Subject: [PATCH] Feature/fix warnings (#110) * Fix warnings * Update docs --- .../ApogeeHeightChangingManeuver_8cpp.html | 1 + ...pogeeHeightChangingManeuver_8h_source.html | 8 +- .../ApsidalAlignmentManeuver_8h_source.html | 8 +- Docs/html/CombinedManeuver_8cpp.html | 1 + Docs/html/CombinedManeuver_8h_source.html | 53 +++-- Docs/html/ConicOrbitalElements_8h_source.html | 4 +- Docs/html/Coordinate_8cpp.html | 1 + Docs/html/Coordinate_8h_source.html | 32 +-- Docs/html/EngineDTO_8h_source.html | 16 +- Docs/html/EquinoctialElements_8h_source.html | 2 +- Docs/html/FrameFile_8cpp.html | 1 + Docs/html/FrameFile_8h_source.html | 8 +- Docs/html/FuelTankDTO_8h_source.html | 4 +- Docs/html/GeometryFinder_8cpp.html | 2 - Docs/html/GeometryFinder_8h_source.html | 10 +- Docs/html/Launch_8h_source.html | 55 +++--- Docs/html/NadirAttitude_8h_source.html | 6 +- 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4 +- .../Attitudes/TowardObjectAttitude.h | 4 +- IO.SDK/Maneuvers/Attitudes/ZenithAttitude.cpp | 4 +- IO.SDK/Maneuvers/Attitudes/ZenithAttitude.h | 4 +- IO.SDK/Maneuvers/CombinedManeuver.cpp | 6 +- IO.SDK/Maneuvers/CombinedManeuver.h | 1 - IO.SDK/Maneuvers/Launch.h | 1 - .../OrbitalPlaneChangingManeuver.cpp | 4 +- .../PerigeeHeightChangingManeuver.cpp | 6 +- .../OrbitalParameters/OrbitalParameters.cpp | 4 +- IO.SDK/OrbitalParameters/OrbitalParameters.h | 2 +- IO.SDK/Propagators/Propagator.cpp | 1 - IO.SDK/Scenario/Scenario.h | 46 +---- IO.SDK/Sites/LaunchSite.cpp | 2 +- 286 files changed, 1360 insertions(+), 1779 deletions(-) diff --git a/Docs/html/ApogeeHeightChangingManeuver_8cpp.html b/Docs/html/ApogeeHeightChangingManeuver_8cpp.html index b4b915eb..046e8afd 100644 --- a/Docs/html/ApogeeHeightChangingManeuver_8cpp.html +++ b/Docs/html/ApogeeHeightChangingManeuver_8cpp.html @@ -88,6 +88,7 @@
#include <ApogeeHeightChangingManeuver.h>
#include <cmath>
+#include <utility>
#include <Parameters.h>

Detailed Description

Author
Sylvain Guillet (sylva.nosp@m.in.g.nosp@m.uille.nosp@m.t@li.nosp@m.ve.co.nosp@m.m)
diff --git a/Docs/html/ApogeeHeightChangingManeuver_8h_source.html b/Docs/html/ApogeeHeightChangingManeuver_8h_source.html index c015b868..58022b22 100644 --- a/Docs/html/ApogeeHeightChangingManeuver_8h_source.html +++ b/Docs/html/ApogeeHeightChangingManeuver_8h_source.html @@ -130,10 +130,10 @@
IO::SDK::Maneuvers::ApogeeHeightChangingManeuver
Definition: ApogeeHeightChangingManeuver.h:28
-
IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: ApogeeHeightChangingManeuver.cpp:30
-
IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::ApogeeHeightChangingManeuver
ApogeeHeightChangingManeuver(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, double targetHeight)
Definition: ApogeeHeightChangingManeuver.cpp:15
-
IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: ApogeeHeightChangingManeuver.cpp:44
-
IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: ApogeeHeightChangingManeuver.cpp:23
+
IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: ApogeeHeightChangingManeuver.cpp:31
+
IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::ApogeeHeightChangingManeuver
ApogeeHeightChangingManeuver(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, double targetHeight)
Definition: ApogeeHeightChangingManeuver.cpp:16
+
IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: ApogeeHeightChangingManeuver.cpp:45
+
IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: ApogeeHeightChangingManeuver.cpp:24
IO::SDK::Maneuvers::ManeuverBase
Maneuverbase class used by concrete maneuvers.
Definition: ManeuverBase.h:36
IO::SDK::OrbitalParameters::OrbitalParameters
Orbital parameters.
Definition: OrbitalParameters.h:34
IO::SDK::OrbitalParameters::StateOrientation
Definition: StateOrientation.h:20
diff --git a/Docs/html/ApsidalAlignmentManeuver_8h_source.html b/Docs/html/ApsidalAlignmentManeuver_8h_source.html index 23eb3f32..944c0431 100644 --- a/Docs/html/ApsidalAlignmentManeuver_8h_source.html +++ b/Docs/html/ApsidalAlignmentManeuver_8h_source.html @@ -138,11 +138,11 @@
89#endif
IO::SDK::Maneuvers::ApsidalAlignmentManeuver
Definition: ApsidalAlignmentManeuver.h:21
-
IO::SDK::Maneuvers::ApsidalAlignmentManeuver::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: ApsidalAlignmentManeuver.cpp:55
-
IO::SDK::Maneuvers::ApsidalAlignmentManeuver::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Definition: ApsidalAlignmentManeuver.cpp:61
+
IO::SDK::Maneuvers::ApsidalAlignmentManeuver::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: ApsidalAlignmentManeuver.cpp:58
+
IO::SDK::Maneuvers::ApsidalAlignmentManeuver::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Definition: ApsidalAlignmentManeuver.cpp:64
IO::SDK::Maneuvers::ApsidalAlignmentManeuver::ApsidalAlignmentManeuver
ApsidalAlignmentManeuver(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, std::shared_ptr< IO::SDK::OrbitalParameters::OrbitalParameters > targetOrbit)
Definition: ApsidalAlignmentManeuver.cpp:17
-
IO::SDK::Maneuvers::ApsidalAlignmentManeuver::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Define maneuver execution condition.
Definition: ApsidalAlignmentManeuver.cpp:25
-
IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetTheta
double GetTheta() const
Get the theta angle.
Definition: ApsidalAlignmentManeuver.cpp:94
+
IO::SDK::Maneuvers::ApsidalAlignmentManeuver::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Define maneuver execution condition.
Definition: ApsidalAlignmentManeuver.cpp:31
+
IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetTheta
double GetTheta() const
Get the theta angle.
Definition: ApsidalAlignmentManeuver.cpp:97
IO::SDK::Maneuvers::ManeuverBase
Maneuverbase class used by concrete maneuvers.
Definition: ManeuverBase.h:36
IO::SDK::Maneuvers::ManeuverBase::GetDeltaV
IO::SDK::Math::Vector3D GetDeltaV() const
Get the maneuver delta V.
Definition: ManeuverBase.cpp:381
IO::SDK::Math::Vector3D
Definition: Vector3D.h:17
diff --git a/Docs/html/CombinedManeuver_8cpp.html b/Docs/html/CombinedManeuver_8cpp.html index 6c24d591..5c0805d4 100644 --- a/Docs/html/CombinedManeuver_8cpp.html +++ b/Docs/html/CombinedManeuver_8cpp.html @@ -90,6 +90,7 @@ #include <ConicOrbitalElements.h>
#include <Vector3D.h>
#include <Parameters.h>
+#include <utility>

Detailed Description

Author
Sylvain Guillet (sylva.nosp@m.in.g.nosp@m.uille.nosp@m.t@li.nosp@m.ve.co.nosp@m.m)
Version
0.x
diff --git a/Docs/html/CombinedManeuver_8h_source.html b/Docs/html/CombinedManeuver_8h_source.html index 0b818c02..ca76ea99 100644 --- a/Docs/html/CombinedManeuver_8h_source.html +++ b/Docs/html/CombinedManeuver_8h_source.html @@ -109,29 +109,28 @@
30 class CombinedManeuver final : public IO::SDK::Maneuvers::ManeuverBase
31 {
32 private:
-
33 double m_relativeInclination{};
-
34 double m_inclination;
-
35 double m_peregeeRadius;
-
36
-
37 [[nodiscard]] IO::SDK::Math::Vector3D GetDeltaV(const IO::SDK::OrbitalParameters::StateVector& sv) const;
-
38
-
39 protected:
-
45 void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override;
-
46
-
53 IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override;
-
54
-
55 public:
-
60 CombinedManeuver(std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator, double inclination, double perigeeRadius);
-
61
-
62 CombinedManeuver(std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator, double inclination, double perigeeRadius, const IO::SDK::Time::TDB &minimumEpoch);
-
63
-
71 bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override;
-
72
-
73 using IO::SDK::Maneuvers::ManeuverBase::GetDeltaV;
-
74 };
-
75}
-
76
-
77#endif
+
33 double m_inclination;
+
34 double m_peregeeRadius;
+
35
+
36 [[nodiscard]] IO::SDK::Math::Vector3D GetDeltaV(const IO::SDK::OrbitalParameters::StateVector& sv) const;
+
37
+
38 protected:
+
44 void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override;
+
45
+
52 IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override;
+
53
+
54 public:
+
59 CombinedManeuver(std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator, double inclination, double perigeeRadius);
+
60
+
61 CombinedManeuver(std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator, double inclination, double perigeeRadius, const IO::SDK::Time::TDB &minimumEpoch);
+
62
+
70 bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override;
+
71
+
72 using IO::SDK::Maneuvers::ManeuverBase::GetDeltaV;
+
73 };
+
74}
+
75
+
76#endif
@@ -141,10 +140,10 @@
IO::SDK::Maneuvers::CombinedManeuver
Definition: CombinedManeuver.h:31
-
IO::SDK::Maneuvers::CombinedManeuver::CombinedManeuver
CombinedManeuver(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, double inclination, double perigeeRadius)
Construct a new Combined Maneuver object.
Definition: CombinedManeuver.cpp:16
-
IO::SDK::Maneuvers::CombinedManeuver::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: CombinedManeuver.cpp:43
-
IO::SDK::Maneuvers::CombinedManeuver::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: CombinedManeuver.cpp:24
-
IO::SDK::Maneuvers::CombinedManeuver::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: CombinedManeuver.cpp:49
+
IO::SDK::Maneuvers::CombinedManeuver::CombinedManeuver
CombinedManeuver(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, double inclination, double perigeeRadius)
Construct a new Combined Maneuver object.
Definition: CombinedManeuver.cpp:18
+
IO::SDK::Maneuvers::CombinedManeuver::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: CombinedManeuver.cpp:45
+
IO::SDK::Maneuvers::CombinedManeuver::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: CombinedManeuver.cpp:26
+
IO::SDK::Maneuvers::CombinedManeuver::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: CombinedManeuver.cpp:51
IO::SDK::Maneuvers::ManeuverBase
Maneuverbase class used by concrete maneuvers.
Definition: ManeuverBase.h:36
IO::SDK::Maneuvers::ManeuverBase::GetDeltaV
IO::SDK::Math::Vector3D GetDeltaV() const
Get the maneuver delta V.
Definition: ManeuverBase.cpp:381
IO::SDK::Math::Vector3D
Definition: Vector3D.h:17
diff --git a/Docs/html/ConicOrbitalElements_8h_source.html b/Docs/html/ConicOrbitalElements_8h_source.html index 278be383..39681787 100644 --- a/Docs/html/ConicOrbitalElements_8h_source.html +++ b/Docs/html/ConicOrbitalElements_8h_source.html @@ -200,8 +200,8 @@
IO::SDK::OrbitalParameters::ConicOrbitalElements::GetRightAscendingNodeLongitude
double GetRightAscendingNodeLongitude() const override
Get ascending node longitude
Definition: ConicOrbitalElements.cpp:79
IO::SDK::OrbitalParameters::ConicOrbitalElements::ConicOrbitalElements
ConicOrbitalElements(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, double perifocalDistance, double eccentricity, double inclination, double ascendingNodeLongitude, double periapsisArgument, double meanAnomaly, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)
Definition: ConicOrbitalElements.cpp:17
IO::SDK::OrbitalParameters::OrbitalParameters
Orbital parameters.
Definition: OrbitalParameters.h:34
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetTrueAnomaly
virtual double GetTrueAnomaly() const
Get the True Anomaly.
Definition: OrbitalParameters.cpp:119
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector() const
Get the State Vector at epoch.
Definition: OrbitalParameters.cpp:124
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetTrueAnomaly
virtual double GetTrueAnomaly() const
Get the True Anomaly.
Definition: OrbitalParameters.cpp:121
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector() const
Get the State Vector at epoch.
Definition: OrbitalParameters.cpp:126
IO::SDK::OrbitalParameters::OrbitalParameters::GetMeanAnomaly
virtual double GetMeanAnomaly() const =0
Get the Mean Anomaly.
IO::SDK::OrbitalParameters::StateVector
State vector class.
Definition: StateVector.h:25
IO::SDK::Time::TDB
Definition: TDB.h:20
diff --git a/Docs/html/Coordinate_8cpp.html b/Docs/html/Coordinate_8cpp.html index 806a030b..b53fc37a 100644 --- a/Docs/html/Coordinate_8cpp.html +++ b/Docs/html/Coordinate_8cpp.html @@ -87,6 +87,7 @@
#include <Coordinate.h>
+#include <utility>
#include "SDKException.h"

Detailed Description

Author
Sylvain Guillet (sylva.nosp@m.in.g.nosp@m.uille.nosp@m.t@li.nosp@m.ve.co.nosp@m.m)
diff --git a/Docs/html/Coordinate_8h_source.html b/Docs/html/Coordinate_8h_source.html index f54b3e51..9ccb47bb 100644 --- a/Docs/html/Coordinate_8h_source.html +++ b/Docs/html/Coordinate_8h_source.html @@ -113,7 +113,7 @@
34
35 public:
36
-
42 explicit Coordinate(const std::string &name);
+
42 explicit Coordinate(std::string name);
43 ~Coordinate() = default;
44
45 Coordinate &operator=(const Coordinate &other)
@@ -139,29 +139,29 @@
70 static Coordinate& RightAscension();
71 static Coordinate& Declination();
72 static Coordinate& Colatitude();
-
73 static Coordinate ToCoordinateType(const std::string &coordinateType) ;
+
73 static Coordinate& ToCoordinateType(const std::string &coordinateType) ;
74 };
75
76} // namespace IO::SDK
77
78#endif
IO::SDK::Coordinate
Definition: Coordinate.h:19
-
IO::SDK::Coordinate::Latitude
static Coordinate & Latitude()
Definition: Coordinate.cpp:60
-
IO::SDK::Coordinate::Coordinate
Coordinate(const std::string &name)
Construct a new Coordinate object.
Definition: Coordinate.cpp:26
+
IO::SDK::Coordinate::Latitude
static Coordinate & Latitude()
Definition: Coordinate.cpp:62
-
IO::SDK::Coordinate::RightAscension
static Coordinate & RightAscension()
Definition: Coordinate.cpp:75
+
IO::SDK::Coordinate::RightAscension
static Coordinate & RightAscension()
Definition: Coordinate.cpp:77
+
IO::SDK::Coordinate::ToCoordinateType
static Coordinate & ToCoordinateType(const std::string &coordinateType)
Definition: Coordinate.cpp:92
IO::SDK::Coordinate::operator=
Coordinate & operator=(const Coordinate &other)
Definition: Coordinate.h:45
-
IO::SDK::Coordinate::ToCharArray
const char * ToCharArray() const
Get char array.
Definition: Coordinate.cpp:30
-
IO::SDK::Coordinate::ToCoordinateType
static Coordinate ToCoordinateType(const std::string &coordinateType)
Definition: Coordinate.cpp:90
-
IO::SDK::Coordinate::X
static Coordinate & X()
Definition: Coordinate.cpp:40
-
IO::SDK::Coordinate::Radius
static Coordinate & Radius()
Definition: Coordinate.cpp:65
-
IO::SDK::Coordinate::Range
static Coordinate & Range()
Definition: Coordinate.cpp:70
-
IO::SDK::Coordinate::Altitude
static Coordinate & Altitude()
Definition: Coordinate.cpp:35
-
IO::SDK::Coordinate::Colatitude
static Coordinate & Colatitude()
Definition: Coordinate.cpp:85
-
IO::SDK::Coordinate::Longitude
static Coordinate & Longitude()
Definition: Coordinate.cpp:55
-
IO::SDK::Coordinate::Z
static Coordinate & Z()
Definition: Coordinate.cpp:50
-
IO::SDK::Coordinate::Declination
static Coordinate & Declination()
Definition: Coordinate.cpp:80
-
IO::SDK::Coordinate::Y
static Coordinate & Y()
Definition: Coordinate.cpp:45
+
IO::SDK::Coordinate::ToCharArray
const char * ToCharArray() const
Get char array.
Definition: Coordinate.cpp:32
+
IO::SDK::Coordinate::X
static Coordinate & X()
Definition: Coordinate.cpp:42
+
IO::SDK::Coordinate::Radius
static Coordinate & Radius()
Definition: Coordinate.cpp:67
+
IO::SDK::Coordinate::Range
static Coordinate & Range()
Definition: Coordinate.cpp:72
+
IO::SDK::Coordinate::Altitude
static Coordinate & Altitude()
Definition: Coordinate.cpp:37
+
IO::SDK::Coordinate::Colatitude
static Coordinate & Colatitude()
Definition: Coordinate.cpp:87
+
IO::SDK::Coordinate::Coordinate
Coordinate(std::string name)
Construct a new Coordinate object.
Definition: Coordinate.cpp:28
+
IO::SDK::Coordinate::Longitude
static Coordinate & Longitude()
Definition: Coordinate.cpp:57
+
IO::SDK::Coordinate::Z
static Coordinate & Z()
Definition: Coordinate.cpp:52
+
IO::SDK::Coordinate::Declination
static Coordinate & Declination()
Definition: Coordinate.cpp:82
+
IO::SDK::Coordinate::Y
static Coordinate & Y()
Definition: Coordinate.cpp:47
IO::SDK
Definition: Aberrations.h:17
diff --git a/Docs/html/EngineDTO_8h_source.html b/Docs/html/EngineDTO_8h_source.html index b6e4aeb0..b51ce63d 100644 --- a/Docs/html/EngineDTO_8h_source.html +++ b/Docs/html/EngineDTO_8h_source.html @@ -93,22 +93,22 @@
5 struct EngineDTO
6 {
7 int id;
-
8 char * serialNumber;
-
9 char * fuelTankSerialNumber;
-
10 char * name;
+
8 const char * serialNumber;
+
9 const char * fuelTankSerialNumber;
+
10 const char * name;
11 double isp;
-
12 double fuelflow;
+
12 double fuelFlow;
13 };
14
15}
IO::SDK::API::DTO
Definition: ApogeeHeightChangingManeuverDTO.h:11
IO::SDK::API::DTO::EngineDTO
Definition: EngineDTO.h:6
IO::SDK::API::DTO::EngineDTO::isp
double isp
Definition: EngineDTO.h:11
-
IO::SDK::API::DTO::EngineDTO::serialNumber
char * serialNumber
Definition: EngineDTO.h:8
-
IO::SDK::API::DTO::EngineDTO::fuelTankSerialNumber
char * fuelTankSerialNumber
Definition: EngineDTO.h:9
-
IO::SDK::API::DTO::EngineDTO::name
char * name
Definition: EngineDTO.h:10
-
IO::SDK::API::DTO::EngineDTO::fuelflow
double fuelflow
Definition: EngineDTO.h:12
+
IO::SDK::API::DTO::EngineDTO::serialNumber
const char * serialNumber
Definition: EngineDTO.h:8
+
IO::SDK::API::DTO::EngineDTO::fuelFlow
double fuelFlow
Definition: EngineDTO.h:12
+
IO::SDK::API::DTO::EngineDTO::fuelTankSerialNumber
const char * fuelTankSerialNumber
Definition: EngineDTO.h:9
IO::SDK::API::DTO::EngineDTO::id
int id
Definition: EngineDTO.h:7
+
IO::SDK::API::DTO::EngineDTO::name
const char * name
Definition: EngineDTO.h:10
diff --git a/Docs/html/EquinoctialElements_8h_source.html b/Docs/html/EquinoctialElements_8h_source.html index bb596c31..7efdc135 100644 --- a/Docs/html/EquinoctialElements_8h_source.html +++ b/Docs/html/EquinoctialElements_8h_source.html @@ -197,7 +197,7 @@
IO::SDK::OrbitalParameters::EquinoctialElements::GetMeanAnomaly
double GetMeanAnomaly() const override
Get mean anomaly at epoch
Definition: EquinoctialElements.cpp:96
IO::SDK::OrbitalParameters::EquinoctialElements::GetL
double GetL() const
Get longitude coefficient
Definition: EquinoctialElements.h:74
IO::SDK::OrbitalParameters::OrbitalParameters
Orbital parameters.
Definition: OrbitalParameters.h:34
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector() const
Get the State Vector at epoch.
Definition: OrbitalParameters.cpp:124
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector() const
Get the State Vector at epoch.
Definition: OrbitalParameters.cpp:126
IO::SDK::OrbitalParameters::OrbitalParameters::GetMeanAnomaly
virtual double GetMeanAnomaly() const =0
Get the Mean Anomaly.
IO::SDK::OrbitalParameters::StateVector
State vector class.
Definition: StateVector.h:25
IO::SDK::Time::TDB
Definition: TDB.h:20
diff --git a/Docs/html/FrameFile_8cpp.html b/Docs/html/FrameFile_8cpp.html index ad17976c..9de02766 100644 --- a/Docs/html/FrameFile_8cpp.html +++ b/Docs/html/FrameFile_8cpp.html @@ -88,6 +88,7 @@
#include <FrameFile.h>
#include <filesystem>
+#include <utility>
#include <SpiceUsr.h>

Detailed Description

Author
Sylvain Guillet (sylva.nosp@m.in.g.nosp@m.uille.nosp@m.t@li.nosp@m.ve.co.nosp@m.m)
diff --git a/Docs/html/FrameFile_8h_source.html b/Docs/html/FrameFile_8h_source.html index 41468759..977863ef 100644 --- a/Docs/html/FrameFile_8h_source.html +++ b/Docs/html/FrameFile_8h_source.html @@ -101,7 +101,7 @@
26 const std::string m_filePath{};
27 bool m_fileExists{ false };
28 bool m_isLoaded{ false };
-
29 FrameFile(const std::string& filePath, const std::string& name);
+
29 FrameFile(const std::string& filePath, std::string name);
30 const std::string m_name{};
31
32 public:
@@ -112,10 +112,10 @@
42}
43#endif
IO::SDK::Frames::FrameFile
Frame file.
Definition: FrameFile.h:23
-
IO::SDK::Frames::FrameFile::GetName
std::string GetName() const
Get the frame name.
Definition: FrameFile.cpp:39
-
IO::SDK::Frames::FrameFile::~FrameFile
virtual ~FrameFile()
Definition: FrameFile.cpp:34
-
IO::SDK::Frames::FrameFile::FrameFile
FrameFile(const std::string &filePath, const std::string &name)
Definition: FrameFile.cpp:15
+
IO::SDK::Frames::FrameFile::GetName
std::string GetName() const
Get the frame name.
Definition: FrameFile.cpp:40
+
IO::SDK::Frames::FrameFile::~FrameFile
virtual ~FrameFile()
Definition: FrameFile.cpp:35
IO::SDK::Frames::FrameFile::m_name
const std::string m_name
Definition: FrameFile.h:30
+
IO::SDK::Frames::FrameFile::FrameFile
FrameFile(const std::string &filePath, std::string name)
Definition: FrameFile.cpp:16
IO::SDK::Frames::FrameFile::m_filePath
const std::string m_filePath
Definition: FrameFile.h:26
IO::SDK::Frames::FrameFile::m_isLoaded
bool m_isLoaded
Definition: FrameFile.h:28
IO::SDK::Frames::FrameFile::m_fileExists
bool m_fileExists
Definition: FrameFile.h:27
diff --git a/Docs/html/FuelTankDTO_8h_source.html b/Docs/html/FuelTankDTO_8h_source.html index 15c64542..cda73655 100644 --- a/Docs/html/FuelTankDTO_8h_source.html +++ b/Docs/html/FuelTankDTO_8h_source.html @@ -93,7 +93,7 @@
5 struct FuelTankDTO
6 {
7 int id;
-
8 char * serialNumber;
+
8 const char * serialNumber;
9
10 double capacity;
11 double quantity;
@@ -102,9 +102,9 @@
IO::SDK::API::DTO
Definition: ApogeeHeightChangingManeuverDTO.h:11
IO::SDK::API::DTO::FuelTankDTO
Definition: FuelTankDTO.h:6
IO::SDK::API::DTO::FuelTankDTO::quantity
double quantity
Definition: FuelTankDTO.h:11
+
IO::SDK::API::DTO::FuelTankDTO::serialNumber
const char * serialNumber
Definition: FuelTankDTO.h:8
IO::SDK::API::DTO::FuelTankDTO::capacity
double capacity
Definition: FuelTankDTO.h:10
IO::SDK::API::DTO::FuelTankDTO::id
int id
Definition: FuelTankDTO.h:7
-
IO::SDK::API::DTO::FuelTankDTO::serialNumber
char * serialNumber
Definition: FuelTankDTO.h:8
diff --git a/Docs/html/GeometryFinder_8cpp.html b/Docs/html/GeometryFinder_8cpp.html index 900e3f88..91879327 100644 --- a/Docs/html/GeometryFinder_8cpp.html +++ b/Docs/html/GeometryFinder_8cpp.html @@ -89,9 +89,7 @@
#include <GeometryFinder.h>
#include <SpiceUsr.h>
#include <Builder.h>
-#include "CelestialBody.h"
#include "IlluminationAngle.h"
-#include <Helpers/Type.cpp>
diff --git a/Docs/html/GeometryFinder_8h_source.html b/Docs/html/GeometryFinder_8h_source.html index b2ac6c22..9f24d26a 100644 --- a/Docs/html/GeometryFinder_8h_source.html +++ b/Docs/html/GeometryFinder_8h_source.html @@ -162,11 +162,11 @@
RelationalOperator.h
Window.h
IO::SDK::Constraints::GeometryFinder
Definition: GeometryFinder.h:25
-
IO::SDK::Constraints::GeometryFinder::FindWindowsOnIlluminationConstraint
static std::vector< IO::SDK::Time::Window< IO::SDK::Time::TDB > > FindWindowsOnIlluminationConstraint(const IO::SDK::Time::Window< IO::SDK::Time::TDB > &searchWindow, int observerId, const std::string &illuminationSource, int targetBody, const std::string &fixedFrame, const double coordinates[3], const IlluminationAngle &illuminationType, const IO::SDK::Constraints::RelationalOperator &relationalOperator, double value, double adjustValue, IO::SDK::AberrationsEnum aberration, const IO::SDK::Time::TimeSpan &stepSize, const std::string &method)
Definition: GeometryFinder.cpp:123
-
IO::SDK::Constraints::GeometryFinder::FindWindowsInFieldOfViewConstraint
static std::vector< IO::SDK::Time::Window< IO::SDK::Time::TDB > > FindWindowsInFieldOfViewConstraint(const IO::SDK::Time::Window< IO::SDK::Time::TDB > &searchWindow, int observerId, int instrumentId, int targetId, const std::string &targetFrame, const std::string &targetShape, IO::SDK::AberrationsEnum aberration, const IO::SDK::Time::TimeSpan &stepSize)
Definition: GeometryFinder.cpp:165
-
IO::SDK::Constraints::GeometryFinder::FindWindowsOnCoordinateConstraint
static std::vector< IO::SDK::Time::Window< IO::SDK::Time::TDB > > FindWindowsOnCoordinateConstraint(const IO::SDK::Time::Window< IO::SDK::Time::TDB > &searchWindow, int observerId, int targetId, const std::string &frame, const IO::SDK::CoordinateSystem &coordinateSystem, const IO::SDK::Coordinate &coordinate, const IO::SDK::Constraints::RelationalOperator &relationalOperator, double value, double adjustValue, IO::SDK::AberrationsEnum aberration, const IO::SDK::Time::TimeSpan &stepSize)
Definition: GeometryFinder.cpp:87
-
IO::SDK::Constraints::GeometryFinder::FindWindowsOnOccultationConstraint
static std::vector< IO::SDK::Time::Window< IO::SDK::Time::TDB > > FindWindowsOnOccultationConstraint(const IO::SDK::Time::Window< IO::SDK::Time::TDB > &searchWindow, int observerId, int targetId, const std::string &targetFrame, const std::string &targetShape, int frontBodyId, const std::string &frontFrame, const std::string &frontShape, const IO::SDK::OccultationType &occultationType, IO::SDK::AberrationsEnum aberration, const IO::SDK::Time::TimeSpan &stepSize)
Definition: GeometryFinder.cpp:47
-
IO::SDK::Constraints::GeometryFinder::FindWindowsOnDistanceConstraint
static std::vector< Time::Window< Time::TDB > > FindWindowsOnDistanceConstraint(const IO::SDK::Time::Window< IO::SDK::Time::TDB > &searchWindow, int observerId, int targetId, const Constraints::RelationalOperator &constraint, double value, IO::SDK::AberrationsEnum aberration, const Time::TimeSpan &stepSize)
Definition: GeometryFinder.cpp:13
+
IO::SDK::Constraints::GeometryFinder::FindWindowsOnIlluminationConstraint
static std::vector< IO::SDK::Time::Window< IO::SDK::Time::TDB > > FindWindowsOnIlluminationConstraint(const IO::SDK::Time::Window< IO::SDK::Time::TDB > &searchWindow, int observerId, const std::string &illuminationSource, int targetBody, const std::string &fixedFrame, const double coordinates[3], const IlluminationAngle &illuminationType, const IO::SDK::Constraints::RelationalOperator &relationalOperator, double value, double adjustValue, IO::SDK::AberrationsEnum aberration, const IO::SDK::Time::TimeSpan &stepSize, const std::string &method)
Definition: GeometryFinder.cpp:121
+
IO::SDK::Constraints::GeometryFinder::FindWindowsInFieldOfViewConstraint
static std::vector< IO::SDK::Time::Window< IO::SDK::Time::TDB > > FindWindowsInFieldOfViewConstraint(const IO::SDK::Time::Window< IO::SDK::Time::TDB > &searchWindow, int observerId, int instrumentId, int targetId, const std::string &targetFrame, const std::string &targetShape, IO::SDK::AberrationsEnum aberration, const IO::SDK::Time::TimeSpan &stepSize)
Definition: GeometryFinder.cpp:163
+
IO::SDK::Constraints::GeometryFinder::FindWindowsOnCoordinateConstraint
static std::vector< IO::SDK::Time::Window< IO::SDK::Time::TDB > > FindWindowsOnCoordinateConstraint(const IO::SDK::Time::Window< IO::SDK::Time::TDB > &searchWindow, int observerId, int targetId, const std::string &frame, const IO::SDK::CoordinateSystem &coordinateSystem, const IO::SDK::Coordinate &coordinate, const IO::SDK::Constraints::RelationalOperator &relationalOperator, double value, double adjustValue, IO::SDK::AberrationsEnum aberration, const IO::SDK::Time::TimeSpan &stepSize)
Definition: GeometryFinder.cpp:85
+
IO::SDK::Constraints::GeometryFinder::FindWindowsOnOccultationConstraint
static std::vector< IO::SDK::Time::Window< IO::SDK::Time::TDB > > FindWindowsOnOccultationConstraint(const IO::SDK::Time::Window< IO::SDK::Time::TDB > &searchWindow, int observerId, int targetId, const std::string &targetFrame, const std::string &targetShape, int frontBodyId, const std::string &frontFrame, const std::string &frontShape, const IO::SDK::OccultationType &occultationType, IO::SDK::AberrationsEnum aberration, const IO::SDK::Time::TimeSpan &stepSize)
Definition: GeometryFinder.cpp:45
+
IO::SDK::Constraints::GeometryFinder::FindWindowsOnDistanceConstraint
static std::vector< Time::Window< Time::TDB > > FindWindowsOnDistanceConstraint(const IO::SDK::Time::Window< IO::SDK::Time::TDB > &searchWindow, int observerId, int targetId, const Constraints::RelationalOperator &constraint, double value, IO::SDK::AberrationsEnum aberration, const Time::TimeSpan &stepSize)
Definition: GeometryFinder.cpp:11
IO::SDK::Constraints::RelationalOperator
Definition: RelationalOperator.h:19
IO::SDK::CoordinateSystem
Definition: CoordinateSystem.h:19
IO::SDK::Coordinate
Definition: Coordinate.h:19
diff --git a/Docs/html/Launch_8h_source.html b/Docs/html/Launch_8h_source.html index 79a1bfd4..6eef1785 100644 --- a/Docs/html/Launch_8h_source.html +++ b/Docs/html/Launch_8h_source.html @@ -121,34 +121,33 @@
42 double m_inertialDescendingAzimuthLaunch{std::numeric_limits<double>::quiet_NaN()};
43 double m_nonInertialDescendingAzimuthLaunch{std::numeric_limits<double>::quiet_NaN()};
44 double m_nonInertialInsertionVelocity{std::numeric_limits<double>::quiet_NaN()};
-
45 double m_inertialInsertionVelocity{std::numeric_limits<double>::quiet_NaN()};
-
46
-
47 const double m_deltaL{std::numeric_limits<double>::quiet_NaN()};
-
48 const double m_inclination{std::numeric_limits<double>::quiet_NaN()};
-
49
-
50 std::vector<LaunchWindow> FindLaunchWindows(const IO::SDK::Time::Window<IO::SDK::Time::UTC> &windowToSearch);
-
51
-
52 public:
-
62 Launch(const IO::SDK::Sites::LaunchSite& launchSite, const IO::SDK::Sites::Site& recoverySite, bool launchByDay, const IO::SDK::OrbitalParameters::OrbitalParameters &targetOrbit);
-
63
-
69 double GetNonInertialAscendingAzimuthLaunch();
-
70
-
76 double GetNonInertialDescendingAzimuthLaunch();
-
77
-
83 double GetInertialAscendingAzimuthLaunch();
-
84
-
90 double GetInertialDescendingAzimuthLaunch();
-
91
-
97 double GetNonInertialInsertionVelocity();
-
98
-
104 double GetInertialInsertionVelocity();
-
105
-
112 std::vector<LaunchWindow> GetLaunchWindows(const IO::SDK::Time::Window<IO::SDK::Time::UTC> &searchWindow);
-
113 };
-
114
-
115} // namespace IO::SDK::Maneuvers
-
116
-
117#endif // LAUNCH_MANEUVER_H
+
45
+
46 const double m_deltaL{std::numeric_limits<double>::quiet_NaN()};
+
47 const double m_inclination{std::numeric_limits<double>::quiet_NaN()};
+
48
+
49 std::vector<LaunchWindow> FindLaunchWindows(const IO::SDK::Time::Window<IO::SDK::Time::UTC> &windowToSearch);
+
50
+
51 public:
+
61 Launch(const IO::SDK::Sites::LaunchSite& launchSite, const IO::SDK::Sites::Site& recoverySite, bool launchByDay, const IO::SDK::OrbitalParameters::OrbitalParameters &targetOrbit);
+
62
+
68 double GetNonInertialAscendingAzimuthLaunch();
+
69
+
75 double GetNonInertialDescendingAzimuthLaunch();
+
76
+
82 double GetInertialAscendingAzimuthLaunch();
+
83
+
89 double GetInertialDescendingAzimuthLaunch();
+
90
+
96 double GetNonInertialInsertionVelocity();
+
97
+
103 double GetInertialInsertionVelocity();
+
104
+
111 std::vector<LaunchWindow> GetLaunchWindows(const IO::SDK::Time::Window<IO::SDK::Time::UTC> &searchWindow);
+
112 };
+
113
+
114} // namespace IO::SDK::Maneuvers
+
115
+
116#endif // LAUNCH_MANEUVER_H
Engine.h
LaunchSite.h
LaunchWindow.h
diff --git a/Docs/html/NadirAttitude_8h_source.html b/Docs/html/NadirAttitude_8h_source.html index 45d9e4e0..97be0c6b 100644 --- a/Docs/html/NadirAttitude_8h_source.html +++ b/Docs/html/NadirAttitude_8h_source.html @@ -113,9 +113,9 @@
45 IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override;
46
47 public:
-
54 NadirAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
+
54 NadirAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*>& engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
55
-
63 NadirAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
+
63 NadirAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*>& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
64
72 bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override;
73 };
@@ -129,7 +129,7 @@
StateOrientation.h
Vector3D.h
IO::SDK::Maneuvers::Attitudes::NadirAttitude
Definition: NadirAttitude.h:27
-
IO::SDK::Maneuvers::Attitudes::NadirAttitude::NadirAttitude
NadirAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
Construct a new Nadir Attitude object.
Definition: NadirAttitude.cpp:13
+
IO::SDK::Maneuvers::Attitudes::NadirAttitude::NadirAttitude
NadirAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
Construct a new Nadir Attitude object.
Definition: NadirAttitude.cpp:13
IO::SDK::Maneuvers::Attitudes::NadirAttitude::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: NadirAttitude.cpp:25
IO::SDK::Maneuvers::Attitudes::NadirAttitude::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: NadirAttitude.cpp:36
IO::SDK::Maneuvers::Attitudes::NadirAttitude::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: NadirAttitude.cpp:30
diff --git a/Docs/html/OrbitalParameters_8cpp.html b/Docs/html/OrbitalParameters_8cpp.html index ac4d3686..66a5b302 100644 --- a/Docs/html/OrbitalParameters_8cpp.html +++ b/Docs/html/OrbitalParameters_8cpp.html @@ -90,6 +90,7 @@ #include <StateVector.h>
#include <InertialFrames.h>
#include <Parameters.h>
+#include <utility>

Detailed Description

Author
Sylvain Guillet (sylva.nosp@m.in.g.nosp@m.uille.nosp@m.t@li.nosp@m.ve.co.nosp@m.m)
Version
0.x
diff --git a/Docs/html/OrbitalParameters_8h_source.html b/Docs/html/OrbitalParameters_8h_source.html index d8e6023e..4d053b78 100644 --- a/Docs/html/OrbitalParameters_8h_source.html +++ b/Docs/html/OrbitalParameters_8h_source.html @@ -114,7 +114,7 @@
39 const IO::SDK::Frames::Frames m_frame;
40
41 public:
-
49 OrbitalParameters(const std::shared_ptr<IO::SDK::Body::CelestialBody> &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame);
+
49 OrbitalParameters(const std::shared_ptr<IO::SDK::Body::CelestialBody> &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame);
50
51 virtual ~OrbitalParameters() = default;
52
@@ -203,41 +203,41 @@
IO::SDK::OrbitalParameters::OrbitalParameters
Orbital parameters.
Definition: OrbitalParameters.h:34
IO::SDK::OrbitalParameters::OrbitalParameters::m_epoch
const IO::SDK::Time::TDB m_epoch
Definition: OrbitalParameters.h:38
IO::SDK::OrbitalParameters::OrbitalParameters::GetInclination
virtual double GetInclination() const =0
Get the Inclination.
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetEccentricityVector
IO::SDK::Math::Vector3D GetEccentricityVector() const
Get the Eccentricity Vector.
Definition: OrbitalParameters.cpp:139
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetTrueAnomaly
virtual double GetTrueAnomaly() const
Get the True Anomaly.
Definition: OrbitalParameters.cpp:119
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetEccentricityVector
IO::SDK::Math::Vector3D GetEccentricityVector() const
Get the Eccentricity Vector.
Definition: OrbitalParameters.cpp:141
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetTrueAnomaly
virtual double GetTrueAnomaly() const
Get the True Anomaly.
Definition: OrbitalParameters.cpp:121
IO::SDK::OrbitalParameters::OrbitalParameters::GetRightAscendingNodeLongitude
virtual double GetRightAscendingNodeLongitude() const =0
Get the Right Ascending Node Longitude.
IO::SDK::OrbitalParameters::OrbitalParameters::GetSemiMajorAxis
virtual double GetSemiMajorAxis() const =0
Get the Semi Major Axis.
IO::SDK::OrbitalParameters::OrbitalParameters::GetSpecificAngularMomentum
virtual IO::SDK::Math::Vector3D GetSpecificAngularMomentum() const =0
Get the Specific Angular Momentum.
+
IO::SDK::OrbitalParameters::OrbitalParameters::OrbitalParameters
OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame)
Construct a new Orbital Parameters object.
Definition: OrbitalParameters.cpp:18
IO::SDK::OrbitalParameters::OrbitalParameters::GetSpecificOrbitalEnergy
virtual double GetSpecificOrbitalEnergy() const =0
Get the Specific Orbital Energy.
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetEccentricAnomaly
virtual double GetEccentricAnomaly(const IO::SDK::Time::TDB &epoch) const
Get the Eccentric Anomaly.
Definition: OrbitalParameters.cpp:84
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetTimeToTrueAnomaly
virtual IO::SDK::Time::TDB GetTimeToTrueAnomaly(double trueAnomalyTarget) const
Get the Time To True Anomaly.
Definition: OrbitalParameters.cpp:65
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetEccentricAnomaly
virtual double GetEccentricAnomaly(const IO::SDK::Time::TDB &epoch) const
Get the Eccentric Anomaly.
Definition: OrbitalParameters.cpp:86
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetTimeToTrueAnomaly
virtual IO::SDK::Time::TDB GetTimeToTrueAnomaly(double trueAnomalyTarget) const
Get the Time To True Anomaly.
Definition: OrbitalParameters.cpp:67
-
IO::SDK::OrbitalParameters::OrbitalParameters::IsElliptical
bool IsElliptical() const
Is elliptical ?
Definition: OrbitalParameters.cpp:25
-
IO::SDK::OrbitalParameters::OrbitalParameters::IsParabolic
bool IsParabolic() const
Is parabolic ?
Definition: OrbitalParameters.cpp:30
+
IO::SDK::OrbitalParameters::OrbitalParameters::IsElliptical
bool IsElliptical() const
Is elliptical ?
Definition: OrbitalParameters.cpp:27
+
IO::SDK::OrbitalParameters::OrbitalParameters::IsParabolic
bool IsParabolic() const
Is parabolic ?
Definition: OrbitalParameters.cpp:32
IO::SDK::OrbitalParameters::OrbitalParameters::GetEccentricity
virtual double GetEccentricity() const =0
Get the Eccentricity.
IO::SDK::OrbitalParameters::OrbitalParameters::GetPeriod
virtual IO::SDK::Time::TimeSpan GetPeriod() const =0
Get the Period.
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetApogeeVector
IO::SDK::Math::Vector3D GetApogeeVector() const
Get the Apogee Vector.
Definition: OrbitalParameters.cpp:150
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetTrueLongitude
double GetTrueLongitude() const
Get the True Longitude.
Definition: OrbitalParameters.cpp:194
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetApogeeVector
IO::SDK::Math::Vector3D GetApogeeVector() const
Get the Apogee Vector.
Definition: OrbitalParameters.cpp:152
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetTrueLongitude
double GetTrueLongitude() const
Get the True Longitude.
Definition: OrbitalParameters.cpp:196
IO::SDK::OrbitalParameters::OrbitalParameters::m_centerOfMotion
const std::shared_ptr< IO::SDK::Body::CelestialBody > m_centerOfMotion
Definition: OrbitalParameters.h:37
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetMeanLongitude
double GetMeanLongitude() const
Get the Mean Longitude.
Definition: OrbitalParameters.cpp:205
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetMeanLongitude
double GetMeanLongitude() const
Get the Mean Longitude.
Definition: OrbitalParameters.cpp:207
IO::SDK::OrbitalParameters::OrbitalParameters::GetPeriapsisArgument
virtual double GetPeriapsisArgument() const =0
Get the Periapsis Argument.
-
IO::SDK::OrbitalParameters::OrbitalParameters::OrbitalParameters
OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)
Construct a new Orbital Parameters object.
Definition: OrbitalParameters.cpp:16
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector() const
Get the State Vector at epoch.
Definition: OrbitalParameters.cpp:124
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetRADec
IO::SDK::Coordinates::RADec GetRADec() const
Get right ascension and declination.
Definition: OrbitalParameters.cpp:169
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector() const
Get the State Vector at epoch.
Definition: OrbitalParameters.cpp:126
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetRADec
IO::SDK::Coordinates::RADec GetRADec() const
Get right ascension and declination.
Definition: OrbitalParameters.cpp:171
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector(const IO::SDK::Time::TDB &epoch) const =0
Get the State Vector at given epoch.
IO::SDK::OrbitalParameters::OrbitalParameters::m_frame
const IO::SDK::Frames::Frames m_frame
Definition: OrbitalParameters.h:39
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetVelocityAtPerigee
double GetVelocityAtPerigee() const
Get the Velocity at Perigee.
Definition: OrbitalParameters.cpp:184
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetVelocityAtApogee
double GetVelocityAtApogee() const
Get the Velocity At Apogee.
Definition: OrbitalParameters.cpp:189
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetAscendingNodeVector
IO::SDK::Math::Vector3D GetAscendingNodeVector() const
Get the Ascending Node Vector.
Definition: OrbitalParameters.cpp:160
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetEpoch
IO::SDK::Time::TDB GetEpoch() const
Get the Epoch.
Definition: OrbitalParameters.cpp:129
-
IO::SDK::OrbitalParameters::OrbitalParameters::IsCircular
bool IsCircular() const
Is circular ?
Definition: OrbitalParameters.cpp:40
-
IO::SDK::OrbitalParameters::OrbitalParameters::IsHyperbolic
bool IsHyperbolic() const
Is hyperbolic ?
Definition: OrbitalParameters.cpp:35
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetMeanMotion
double GetMeanMotion() const
Get the Mean Motion.
Definition: OrbitalParameters.cpp:45
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetTimeToMeanAnomaly
virtual IO::SDK::Time::TDB GetTimeToMeanAnomaly(double meanAnomalyTarget) const
Get the Time To Mean Anomaly.
Definition: OrbitalParameters.cpp:55
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetPerigeeVector
IO::SDK::Math::Vector3D GetPerigeeVector() const
Get the Perigee Vector.
Definition: OrbitalParameters.cpp:145
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetFrame
const IO::SDK::Frames::Frames & GetFrame() const
Get the Frame.
Definition: OrbitalParameters.cpp:134
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetVelocityAtPerigee
double GetVelocityAtPerigee() const
Get the Velocity at Perigee.
Definition: OrbitalParameters.cpp:186
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetVelocityAtApogee
double GetVelocityAtApogee() const
Get the Velocity At Apogee.
Definition: OrbitalParameters.cpp:191
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetAscendingNodeVector
IO::SDK::Math::Vector3D GetAscendingNodeVector() const
Get the Ascending Node Vector.
Definition: OrbitalParameters.cpp:162
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetEpoch
IO::SDK::Time::TDB GetEpoch() const
Get the Epoch.
Definition: OrbitalParameters.cpp:131
+
IO::SDK::OrbitalParameters::OrbitalParameters::IsCircular
bool IsCircular() const
Is circular ?
Definition: OrbitalParameters.cpp:42
+
IO::SDK::OrbitalParameters::OrbitalParameters::IsHyperbolic
bool IsHyperbolic() const
Is hyperbolic ?
Definition: OrbitalParameters.cpp:37
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetMeanMotion
double GetMeanMotion() const
Get the Mean Motion.
Definition: OrbitalParameters.cpp:47
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetTimeToMeanAnomaly
virtual IO::SDK::Time::TDB GetTimeToMeanAnomaly(double meanAnomalyTarget) const
Get the Time To Mean Anomaly.
Definition: OrbitalParameters.cpp:57
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetPerigeeVector
IO::SDK::Math::Vector3D GetPerigeeVector() const
Get the Perigee Vector.
Definition: OrbitalParameters.cpp:147
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetFrame
const IO::SDK::Frames::Frames & GetFrame() const
Get the Frame.
Definition: OrbitalParameters.cpp:136
IO::SDK::OrbitalParameters::OrbitalParameters::GetMeanAnomaly
virtual double GetMeanAnomaly() const =0
Get the Mean Anomaly.
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetCenterOfMotion
const std::shared_ptr< IO::SDK::Body::CelestialBody > & GetCenterOfMotion() const
Get the Center Of Motion.
Definition: OrbitalParameters.cpp:20
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetCenterOfMotion
const std::shared_ptr< IO::SDK::Body::CelestialBody > & GetCenterOfMotion() const
Get the Center Of Motion.
Definition: OrbitalParameters.cpp:22
IO::SDK::OrbitalParameters::StateVector
State vector class.
Definition: StateVector.h:25
IO::SDK::Time::TDB
Definition: TDB.h:20
IO::SDK::Time::TimeSpan
Definition: TimeSpan.h:19
diff --git a/Docs/html/OrbitalPlaneChangingManeuverDTO_8h_source.html b/Docs/html/OrbitalPlaneChangingManeuverDTO_8h_source.html index 92526720..4c629a52 100644 --- a/Docs/html/OrbitalPlaneChangingManeuverDTO_8h_source.html +++ b/Docs/html/OrbitalPlaneChangingManeuverDTO_8h_source.html @@ -101,7 +101,7 @@
13 struct OrbitalPlaneChangingManeuverDTO
14 {
15 int maneuverOrder{-1};
-
16 char* engines[5]{};
+
16 const char* engines[5]{};
17 double attitudeHoldDuration{0.0};
18 double minimumEpoch{0.0};
19
@@ -125,7 +125,7 @@
IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO::attitudeWindow
WindowDTO attitudeWindow
Definition: OrbitalPlaneChangingManeuverDTO.h:24
IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO::maneuverOrder
int maneuverOrder
Definition: OrbitalPlaneChangingManeuverDTO.h:15
IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO::deltaV
Vector3DDTO deltaV
Definition: OrbitalPlaneChangingManeuverDTO.h:25
-
IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO::engines
char * engines[5]
Definition: OrbitalPlaneChangingManeuverDTO.h:16
+
IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO::engines
const char * engines[5]
Definition: OrbitalPlaneChangingManeuverDTO.h:16
IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO::thrustWindow
WindowDTO thrustWindow
Definition: OrbitalPlaneChangingManeuverDTO.h:23
IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO::minimumEpoch
double minimumEpoch
Definition: OrbitalPlaneChangingManeuverDTO.h:18
IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO::targetOrbit
StateVectorDTO targetOrbit
Definition: OrbitalPlaneChangingManeuverDTO.h:20
diff --git a/Docs/html/PerigeeHeightChangingManeuver_8cpp.html b/Docs/html/PerigeeHeightChangingManeuver_8cpp.html index 2b8c434c..186e6dd9 100644 --- a/Docs/html/PerigeeHeightChangingManeuver_8cpp.html +++ b/Docs/html/PerigeeHeightChangingManeuver_8cpp.html @@ -89,6 +89,7 @@
#include <PerigeeHeightChangingManeuver.h>
#include <Constants.h>
#include <Parameters.h>
+#include <utility>

Detailed Description

Author
Sylvain Guillet (sylva.nosp@m.in.g.nosp@m.uille.nosp@m.t@li.nosp@m.ve.co.nosp@m.m)
Version
0.x
diff --git a/Docs/html/PerigeeHeightChangingManeuver_8h_source.html b/Docs/html/PerigeeHeightChangingManeuver_8h_source.html index ae900acf..8031d65d 100644 --- a/Docs/html/PerigeeHeightChangingManeuver_8h_source.html +++ b/Docs/html/PerigeeHeightChangingManeuver_8h_source.html @@ -117,10 +117,10 @@
IO::SDK::Maneuvers::ManeuverBase
Maneuverbase class used by concrete maneuvers.
Definition: ManeuverBase.h:36
IO::SDK::Maneuvers::PerigeeHeightChangingManeuver
Definition: PerigeeHeightChangingManeuver.h:19
-
IO::SDK::Maneuvers::PerigeeHeightChangingManeuver::PerigeeHeightChangingManeuver
PerigeeHeightChangingManeuver(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, double targetHeight)
Construct a new Perigee Height Changing Maneuver object.
Definition: PerigeeHeightChangingManeuver.cpp:15
-
IO::SDK::Maneuvers::PerigeeHeightChangingManeuver::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: PerigeeHeightChangingManeuver.cpp:54
-
IO::SDK::Maneuvers::PerigeeHeightChangingManeuver::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: PerigeeHeightChangingManeuver.cpp:29
-
IO::SDK::Maneuvers::PerigeeHeightChangingManeuver::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: PerigeeHeightChangingManeuver.cpp:39
+
IO::SDK::Maneuvers::PerigeeHeightChangingManeuver::PerigeeHeightChangingManeuver
PerigeeHeightChangingManeuver(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, double targetHeight)
Construct a new Perigee Height Changing Maneuver object.
Definition: PerigeeHeightChangingManeuver.cpp:17
+
IO::SDK::Maneuvers::PerigeeHeightChangingManeuver::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: PerigeeHeightChangingManeuver.cpp:56
+
IO::SDK::Maneuvers::PerigeeHeightChangingManeuver::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: PerigeeHeightChangingManeuver.cpp:31
+
IO::SDK::Maneuvers::PerigeeHeightChangingManeuver::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: PerigeeHeightChangingManeuver.cpp:41
IO::SDK::OrbitalParameters::OrbitalParameters
Orbital parameters.
Definition: OrbitalParameters.h:34
IO::SDK::OrbitalParameters::StateOrientation
Definition: StateOrientation.h:20
IO::SDK::Propagators::Propagator
Definition: Propagator.h:25
diff --git a/Docs/html/ProgradeAttitude_8h_source.html b/Docs/html/ProgradeAttitude_8h_source.html index e79e288c..b08dd031 100644 --- a/Docs/html/ProgradeAttitude_8h_source.html +++ b/Docs/html/ProgradeAttitude_8h_source.html @@ -112,9 +112,9 @@
44 IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override;
45
46 public:
-
53 ProgradeAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
+
53 ProgradeAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*>& engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
54
-
62 ProgradeAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
+
62 ProgradeAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*>& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
63
71 bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override;
72 };
@@ -128,7 +128,7 @@
IO::SDK::Maneuvers::Attitudes::ProgradeAttitude
Definition: ProgradeAttitude.h:26
IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: ProgradeAttitude.cpp:25
-
IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::ProgradeAttitude
ProgradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
Construct a new Prograde Attitude object.
Definition: ProgradeAttitude.cpp:13
+
IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::ProgradeAttitude
ProgradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
Construct a new Prograde Attitude object.
Definition: ProgradeAttitude.cpp:13
IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: ProgradeAttitude.cpp:30
IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: ProgradeAttitude.cpp:36
IO::SDK::Maneuvers::ManeuverBase
Maneuverbase class used by concrete maneuvers.
Definition: ManeuverBase.h:36
diff --git a/Docs/html/Propagator_8cpp.html b/Docs/html/Propagator_8cpp.html index dd5aa5ce..f262fc74 100644 --- a/Docs/html/Propagator_8cpp.html +++ b/Docs/html/Propagator_8cpp.html @@ -88,7 +88,6 @@
#include <Propagator.h>
#include <PropagatorException.h>
-#include <algorithm>
#include <ManeuverBase.h>
#include <StateOrientation.h>

Detailed Description

diff --git a/Docs/html/Propagator_8h_source.html b/Docs/html/Propagator_8h_source.html index ac7627ef..227ac361 100644 --- a/Docs/html/Propagator_8h_source.html +++ b/Docs/html/Propagator_8h_source.html @@ -145,17 +145,17 @@
IO::SDK::OrbitalParameters::StateOrientation
Definition: StateOrientation.h:20
IO::SDK::OrbitalParameters::StateVector
State vector class.
Definition: StateVector.h:25
IO::SDK::Propagators::Propagator
Definition: Propagator.h:25
-
IO::SDK::Propagators::Propagator::SetStandbyManeuver
void SetStandbyManeuver(IO::SDK::Maneuvers::ManeuverBase *standbyManeuver)
Set the Standby Maneuver.
Definition: Propagator.cpp:26
-
IO::SDK::Propagators::Propagator::ClearStateOrientations
void ClearStateOrientations()
Definition: Propagator.cpp:151
-
IO::SDK::Propagators::Propagator::Propagator
Propagator(const IO::SDK::Body::Spacecraft::Spacecraft &spacecraft, const IO::SDK::Integrators::IntegratorBase &integrator, const IO::SDK::Time::Window< IO::SDK::Time::TDB > &window)
Construct a new Propagator Base object.
Definition: Propagator.cpp:19
-
IO::SDK::Propagators::Propagator::FindNearestLowerStateVector
const IO::SDK::OrbitalParameters::StateVector * FindNearestLowerStateVector(const IO::SDK::Time::TDB &epoch) const
Find the nearest lower state vector from an epoch.
Definition: Propagator.cpp:75
-
IO::SDK::Propagators::Propagator::EraseDataFromEpochToEnd
void EraseDataFromEpochToEnd(const IO::SDK::Time::DateTime &epoch)
Erase data from a given epoch up to end.
Definition: Propagator.cpp:114
-
IO::SDK::Propagators::Propagator::Propagate
void Propagate()
Propagate.
Definition: Propagator.cpp:31
-
IO::SDK::Propagators::Propagator::AddStateOrientation
void AddStateOrientation(const IO::SDK::OrbitalParameters::StateOrientation &so)
Add a state orientation.
Definition: Propagator.cpp:104
-
IO::SDK::Propagators::Propagator::GetLatestStateOrientation
const IO::SDK::OrbitalParameters::StateOrientation * GetLatestStateOrientation() const
Get the Latest State Orientation.
Definition: Propagator.cpp:136
-
IO::SDK::Propagators::Propagator::AddStateVector
void AddStateVector(const IO::SDK::OrbitalParameters::StateVector &sv)
Add a state vector.
Definition: Propagator.cpp:95
-
IO::SDK::Propagators::Propagator::GetStateOrientations
const std::vector< std::vector< IO::SDK::OrbitalParameters::StateOrientation > > & GetStateOrientations() const
Definition: Propagator.cpp:146
-
IO::SDK::Propagators::Propagator::GetStateVectors
const std::vector< IO::SDK::OrbitalParameters::StateVector > & GetStateVectors() const
Get the State Vectors generated by propagator.
Definition: Propagator.cpp:131
+
IO::SDK::Propagators::Propagator::SetStandbyManeuver
void SetStandbyManeuver(IO::SDK::Maneuvers::ManeuverBase *standbyManeuver)
Set the Standby Maneuver.
Definition: Propagator.cpp:25
+
IO::SDK::Propagators::Propagator::ClearStateOrientations
void ClearStateOrientations()
Definition: Propagator.cpp:150
+
IO::SDK::Propagators::Propagator::Propagator
Propagator(const IO::SDK::Body::Spacecraft::Spacecraft &spacecraft, const IO::SDK::Integrators::IntegratorBase &integrator, const IO::SDK::Time::Window< IO::SDK::Time::TDB > &window)
Construct a new Propagator Base object.
Definition: Propagator.cpp:18
+
IO::SDK::Propagators::Propagator::FindNearestLowerStateVector
const IO::SDK::OrbitalParameters::StateVector * FindNearestLowerStateVector(const IO::SDK::Time::TDB &epoch) const
Find the nearest lower state vector from an epoch.
Definition: Propagator.cpp:74
+
IO::SDK::Propagators::Propagator::EraseDataFromEpochToEnd
void EraseDataFromEpochToEnd(const IO::SDK::Time::DateTime &epoch)
Erase data from a given epoch up to end.
Definition: Propagator.cpp:113
+
IO::SDK::Propagators::Propagator::Propagate
void Propagate()
Propagate.
Definition: Propagator.cpp:30
+
IO::SDK::Propagators::Propagator::AddStateOrientation
void AddStateOrientation(const IO::SDK::OrbitalParameters::StateOrientation &so)
Add a state orientation.
Definition: Propagator.cpp:103
+
IO::SDK::Propagators::Propagator::GetLatestStateOrientation
const IO::SDK::OrbitalParameters::StateOrientation * GetLatestStateOrientation() const
Get the Latest State Orientation.
Definition: Propagator.cpp:135
+
IO::SDK::Propagators::Propagator::AddStateVector
void AddStateVector(const IO::SDK::OrbitalParameters::StateVector &sv)
Add a state vector.
Definition: Propagator.cpp:94
+
IO::SDK::Propagators::Propagator::GetStateOrientations
const std::vector< std::vector< IO::SDK::OrbitalParameters::StateOrientation > > & GetStateOrientations() const
Definition: Propagator.cpp:145
+
IO::SDK::Propagators::Propagator::GetStateVectors
const std::vector< IO::SDK::OrbitalParameters::StateVector > & GetStateVectors() const
Get the State Vectors generated by propagator.
Definition: Propagator.cpp:130
IO::SDK::Time::DateTime
Definition: DateTime.h:22
IO::SDK::Time::TDB
Definition: TDB.h:20
diff --git a/Docs/html/Proxy_8h_source.html b/Docs/html/Proxy_8h_source.html index 4e587030..9c686bea 100644 --- a/Docs/html/Proxy_8h_source.html +++ b/Docs/html/Proxy_8h_source.html @@ -171,7 +171,7 @@
216#ifdef __cplusplus
217}
218#endif
-
219#pragma endregion
+
219#pragma endregion Proxy
220
221#ifndef PROXY_H
222#define PROXY_H
diff --git a/Docs/html/RelationalOperator_8h_source.html b/Docs/html/RelationalOperator_8h_source.html index f93c4a53..4d485fbd 100644 --- a/Docs/html/RelationalOperator_8h_source.html +++ b/Docs/html/RelationalOperator_8h_source.html @@ -135,18 +135,18 @@
66
67#endif
IO::SDK::Constraints::RelationalOperator
Definition: RelationalOperator.h:19
-
IO::SDK::Constraints::RelationalOperator::ToCharArray
const char * ToCharArray() const
Get char array constraint name.
Definition: RelationnalOperator.cpp:29
-
IO::SDK::Constraints::RelationalOperator::Equal
static IO::SDK::Constraints::RelationalOperator & Equal()
Definition: RelationnalOperator.cpp:44
-
IO::SDK::Constraints::RelationalOperator::operator=
IO::SDK::Constraints::RelationalOperator & operator=(const RelationalOperator &other)
Definition: RelationnalOperator.cpp:69
-
IO::SDK::Constraints::RelationalOperator::AbsMin
static IO::SDK::Constraints::RelationalOperator & AbsMin()
Definition: RelationnalOperator.cpp:49
-
IO::SDK::Constraints::RelationalOperator::RelationalOperator
RelationalOperator(std::string name)
Construct a new RelationalOperator object.
Definition: RelationnalOperator.cpp:25
-
IO::SDK::Constraints::RelationalOperator::GreaterThan
static IO::SDK::Constraints::RelationalOperator & GreaterThan()
Definition: RelationnalOperator.cpp:34
+
IO::SDK::Constraints::RelationalOperator::ToCharArray
const char * ToCharArray() const
Get char array constraint name.
Definition: RelationnalOperator.cpp:28
+
IO::SDK::Constraints::RelationalOperator::Equal
static IO::SDK::Constraints::RelationalOperator & Equal()
Definition: RelationnalOperator.cpp:43
+
IO::SDK::Constraints::RelationalOperator::operator=
IO::SDK::Constraints::RelationalOperator & operator=(const RelationalOperator &other)
Definition: RelationnalOperator.cpp:68
+
IO::SDK::Constraints::RelationalOperator::AbsMin
static IO::SDK::Constraints::RelationalOperator & AbsMin()
Definition: RelationnalOperator.cpp:48
+
IO::SDK::Constraints::RelationalOperator::RelationalOperator
RelationalOperator(std::string name)
Construct a new RelationalOperator object.
Definition: RelationnalOperator.cpp:24
+
IO::SDK::Constraints::RelationalOperator::GreaterThan
static IO::SDK::Constraints::RelationalOperator & GreaterThan()
Definition: RelationnalOperator.cpp:33
IO::SDK::Constraints::RelationalOperator::RelationalOperator
RelationalOperator(const RelationalOperator &relationalOperator)=default
-
IO::SDK::Constraints::RelationalOperator::LocalMax
static IO::SDK::Constraints::RelationalOperator & LocalMax()
Definition: RelationnalOperator.cpp:64
-
IO::SDK::Constraints::RelationalOperator::AbsMax
static IO::SDK::Constraints::RelationalOperator & AbsMax()
Definition: RelationnalOperator.cpp:54
-
IO::SDK::Constraints::RelationalOperator::LocalMin
static IO::SDK::Constraints::RelationalOperator & LocalMin()
Definition: RelationnalOperator.cpp:59
-
IO::SDK::Constraints::RelationalOperator::LowerThan
static IO::SDK::Constraints::RelationalOperator & LowerThan()
Definition: RelationnalOperator.cpp:39
-
IO::SDK::Constraints::RelationalOperator::ToRelationalOperator
static IO::SDK::Constraints::RelationalOperator ToRelationalOperator(const std::string &relationalOperator)
Definition: RelationnalOperator.cpp:77
+
IO::SDK::Constraints::RelationalOperator::LocalMax
static IO::SDK::Constraints::RelationalOperator & LocalMax()
Definition: RelationnalOperator.cpp:63
+
IO::SDK::Constraints::RelationalOperator::AbsMax
static IO::SDK::Constraints::RelationalOperator & AbsMax()
Definition: RelationnalOperator.cpp:53
+
IO::SDK::Constraints::RelationalOperator::LocalMin
static IO::SDK::Constraints::RelationalOperator & LocalMin()
Definition: RelationnalOperator.cpp:58
+
IO::SDK::Constraints::RelationalOperator::LowerThan
static IO::SDK::Constraints::RelationalOperator & LowerThan()
Definition: RelationnalOperator.cpp:38
+
IO::SDK::Constraints::RelationalOperator::ToRelationalOperator
static IO::SDK::Constraints::RelationalOperator ToRelationalOperator(const std::string &relationalOperator)
Definition: RelationnalOperator.cpp:76
IO::SDK::Constraints
Definition: GeometryFinder.h:22
diff --git a/Docs/html/RelationnalOperator_8cpp.html b/Docs/html/RelationnalOperator_8cpp.html index d47191cd..eb4798db 100644 --- a/Docs/html/RelationnalOperator_8cpp.html +++ b/Docs/html/RelationnalOperator_8cpp.html @@ -88,7 +88,6 @@
#include "RelationalOperator.h"
#include <utility>
-#include <cstring>
#include <SDKException.h>
diff --git a/Docs/html/RetrogradeAttitude_8h_source.html b/Docs/html/RetrogradeAttitude_8h_source.html index bf2d8227..c5ea46cc 100644 --- a/Docs/html/RetrogradeAttitude_8h_source.html +++ b/Docs/html/RetrogradeAttitude_8h_source.html @@ -112,9 +112,9 @@
44 IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override;
45
46 public:
-
53 RetrogradeAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
+
53 RetrogradeAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*>& engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
54
-
62 RetrogradeAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
+
62 RetrogradeAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*>& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration);
63
71 bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override;
72 };
@@ -127,7 +127,7 @@
Propagator.h
Vector3D.h
IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude
Definition: RetrogradeAttitude.h:26
-
IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::RetrogradeAttitude
RetrogradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
Construct a new Retrograde Attitude object.
Definition: RetrogradeAttitude.cpp:13
+
IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::RetrogradeAttitude
RetrogradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
Construct a new Retrograde Attitude object.
Definition: RetrogradeAttitude.cpp:13
IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: RetrogradeAttitude.cpp:26
IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: RetrogradeAttitude.cpp:31
IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: RetrogradeAttitude.cpp:21
diff --git a/Docs/html/ScenarioDTO_8h_source.html b/Docs/html/ScenarioDTO_8h_source.html index 45b460d7..cb822284 100644 --- a/Docs/html/ScenarioDTO_8h_source.html +++ b/Docs/html/ScenarioDTO_8h_source.html @@ -97,7 +97,7 @@
9{
10 struct ScenarioDTO
11 {
-
12 char *Name{};
+
12 const char *Name{};
13 WindowDTO Window{};
14 SpacecraftDTO Spacecraft;
15 SiteDTO Sites[10];
@@ -117,9 +117,9 @@
IO::SDK::API::DTO::ScenarioDTO
Definition: ScenarioDTO.h:11
IO::SDK::API::DTO::ScenarioDTO::CelestialBodies
CelestialBodyDTO CelestialBodies[10]
Definition: ScenarioDTO.h:20
IO::SDK::API::DTO::ScenarioDTO::Spacecraft
SpacecraftDTO Spacecraft
Definition: ScenarioDTO.h:14
+
IO::SDK::API::DTO::ScenarioDTO::Name
const char * Name
Definition: ScenarioDTO.h:12
IO::SDK::API::DTO::ScenarioDTO::Sites
SiteDTO Sites[10]
Definition: ScenarioDTO.h:15
IO::SDK::API::DTO::ScenarioDTO::Window
WindowDTO Window
Definition: ScenarioDTO.h:13
-
IO::SDK::API::DTO::ScenarioDTO::Name
char * Name
Definition: ScenarioDTO.h:12
IO::SDK::API::DTO::SiteDTO
Definition: SiteDTO.h:16
IO::SDK::API::DTO::SpacecraftDTO
Definition: SpacecraftDTO.h:25
IO::SDK::API::DTO::WindowDTO
Definition: WindowDTO.h:7
diff --git a/Docs/html/Scenario_8h_source.html b/Docs/html/Scenario_8h_source.html index 44480865..85648399 100644 --- a/Docs/html/Scenario_8h_source.html +++ b/Docs/html/Scenario_8h_source.html @@ -165,28 +165,12 @@
113 inline Propagators::Propagator &GetPropagator()
114 { return *m_propagator; }
115
-
116
-
117
-
122 void AddDistanceConstraint(Constraints::Parameters::DistanceParameters *distanceParameters);
+
119 void Execute();
+
120 };
+
121
+
122} // IO::SDK
123
-
128 void AddOccultationConstraint(IO::SDK::Constraints::Parameters::OccultationParameters *occultationParameters);
-
129
-
134 void AddDayConstraint(IO::SDK::Constraints::Parameters::ByDayParameters *byDayParameters);
-
135
-
140 void AddNightConstraint(IO::SDK::Constraints::Parameters::ByNightParameters *byNightParameters);
-
141
-
146 void AddBodyVisibilityConstraint(IO::SDK::Constraints::Parameters::BodyVisibilityFromSiteParameters *bodyVisibilityParameters);
-
147
-
152 void AddInFieldOfViewConstraint(IO::SDK::Constraints::Parameters::InFieldOfViewParameters *inFieldOfViewParameters);
-
153
-
158 void AddLaunchConstraint(IO::SDK::Constraints::Parameters::LaunchParameters *launchParameters);
-
159
-
163 void Execute();
-
164 };
-
165
-
166} // IO::SDK
-
167
-
168#endif //IOSDK_SCENARIO_H
+
124#endif //IOSDK_SCENARIO_H
LaunchWindow.h
Propagator.h
VVIntegrator.h
@@ -196,24 +180,17 @@
IO::SDK::Integrators::VVIntegrator
Definition: VVIntegrator.h:37
IO::SDK::Propagators::Propagator
Definition: Propagator.h:25
IO::SDK::Scenario
Definition: Scenario.h:39
-
IO::SDK::Scenario::AddInFieldOfViewConstraint
void AddInFieldOfViewConstraint(IO::SDK::Constraints::Parameters::InFieldOfViewParameters *inFieldOfViewParameters)
IO::SDK::Scenario::GetSites
const std::vector< const IO::SDK::Sites::Site * > & GetSites()
Definition: Scenario.h:106
IO::SDK::Scenario::GetWindow
const IO::SDK::Time::Window< IO::SDK::Time::UTC > & GetWindow() const
Definition: Scenario.h:85
-
IO::SDK::Scenario::AddDistanceConstraint
void AddDistanceConstraint(Constraints::Parameters::DistanceParameters *distanceParameters)
-
IO::SDK::Scenario::AddBodyVisibilityConstraint
void AddBodyVisibilityConstraint(IO::SDK::Constraints::Parameters::BodyVisibilityFromSiteParameters *bodyVisibilityParameters)
-
IO::SDK::Scenario::AddLaunchConstraint
void AddLaunchConstraint(IO::SDK::Constraints::Parameters::LaunchParameters *launchParameters)
IO::SDK::Scenario::Execute
void Execute()
Definition: Scenario.cpp:34
IO::SDK::Scenario::GetCelestialBodies
const std::vector< const IO::SDK::Body::CelestialBody * > & GetCelestialBodies()
Definition: Scenario.h:92
IO::SDK::Scenario::GetSpacecraft
const IO::SDK::Body::Spacecraft::Spacecraft * GetSpacecraft()
Definition: Scenario.h:99
IO::SDK::Scenario::AddCelestialBody
void AddCelestialBody(const IO::SDK::Body::CelestialBody &celestialBody)
Definition: Scenario.cpp:29
IO::SDK::Scenario::Scenario
Scenario(std::string name, const IO::SDK::Time::Window< IO::SDK::Time::UTC > &windows)
Definition: Scenario.cpp:10
IO::SDK::Scenario::AddSite
void AddSite(const IO::SDK::Sites::Site &site)
Definition: Scenario.cpp:17
-
IO::SDK::Scenario::AddDayConstraint
void AddDayConstraint(IO::SDK::Constraints::Parameters::ByDayParameters *byDayParameters)
IO::SDK::Scenario::GetName
std::string GetName() const
Definition: Scenario.h:78
-
IO::SDK::Scenario::AddOccultationConstraint
void AddOccultationConstraint(IO::SDK::Constraints::Parameters::OccultationParameters *occultationParameters)
IO::SDK::Scenario::AttachSpacecraft
void AttachSpacecraft(const IO::SDK::Body::Spacecraft::Spacecraft &spacecraft)
Definition: Scenario.cpp:22
IO::SDK::Scenario::GetPropagator
Propagators::Propagator & GetPropagator()
Definition: Scenario.h:113
-
IO::SDK::Scenario::AddNightConstraint
void AddNightConstraint(IO::SDK::Constraints::Parameters::ByNightParameters *byNightParameters)
IO::SDK::Sites::Site
Site class.
Definition: Site.h:35
IO::SDK::Time::Window< IO::SDK::Time::UTC >
IO::SDK::Constraints::Parameters
Definition: Scenario.h:20
diff --git a/Docs/html/Spacecraft_8h_source.html b/Docs/html/Spacecraft_8h_source.html index bf6ee1b0..af6245e5 100644 --- a/Docs/html/Spacecraft_8h_source.html +++ b/Docs/html/Spacecraft_8h_source.html @@ -231,8 +231,8 @@
337
342 const std::unique_ptr<IO::SDK::Frames::SpacecraftFrameFile> &GetFrame() const;
343
-
344 inline double GetMaximumOperatingMass()
-
345 { return m_maximumOperatingMass; }
+
344 inline double GetMaximumOperatingMass() const
+
345 { return m_maximumOperatingMass; }
346 };
347}
348
@@ -271,6 +271,7 @@
IO::SDK::Body::Spacecraft::Spacecraft::ReadEphemerisKernelComment
std::string ReadEphemerisKernelComment() const
Read ephemeris kernel comment.
Definition: Spacecraft.cpp:111
IO::SDK::Body::Spacecraft::Spacecraft::Right
const IO::SDK::Math::Vector3D Right
Definition: Spacecraft.h:71
IO::SDK::Body::Spacecraft::Spacecraft::GetFrame
const std::unique_ptr< IO::SDK::Frames::SpacecraftFrameFile > & GetFrame() const
Definition: Spacecraft.cpp:316
+
IO::SDK::Body::Spacecraft::Spacecraft::GetMaximumOperatingMass
double GetMaximumOperatingMass() const
Definition: Spacecraft.h:344
IO::SDK::Body::Spacecraft::Spacecraft::GetOrientation
IO::SDK::OrbitalParameters::StateOrientation GetOrientation(const IO::SDK::Time::TDB &epoch, const IO::SDK::Time::TimeSpan &tolerance, const IO::SDK::Frames::Frames &frame) const
Get the Orientation object.
Definition: Spacecraft.cpp:59
IO::SDK::Body::Spacecraft::Spacecraft::GetFilesPath
std::string GetFilesPath() const
Get the Files Path object.
Definition: Spacecraft.h:116
IO::SDK::Body::Spacecraft::Spacecraft::AddFuelTank
void AddFuelTank(const std::string &serialNumber, double capacity, double quantity)
Add a fuel tank.
Definition: Spacecraft.cpp:192
@@ -280,7 +281,6 @@
IO::SDK::Body::Spacecraft::Spacecraft::GetMass
double GetMass() const override
Get the toal mass.
Definition: Spacecraft.cpp:248
IO::SDK::Body::Spacecraft::Spacecraft::Bottom
const IO::SDK::Math::Vector3D Bottom
Definition: Spacecraft.h:72
IO::SDK::Body::Spacecraft::Spacecraft::AddEngine
void AddEngine(const std::string &serialNumber, const std::string &name, const std::string &fuelTankSerialNumber, const Math::Vector3D &position, const Math::Vector3D &orientation, double isp, double fuelFlow)
Add an engine.
Definition: Spacecraft.cpp:208
-
IO::SDK::Body::Spacecraft::Spacecraft::GetMaximumOperatingMass
double GetMaximumOperatingMass()
Definition: Spacecraft.h:344
IO::SDK::Body::Spacecraft::Spacecraft::WriteOrientationKernelComment
void WriteOrientationKernelComment(const std::string &comment) const
Write comment in orientation kernel.
Definition: Spacecraft.cpp:66
IO::SDK::Body::Spacecraft::Spacecraft::GetInstrument
const IO::SDK::Instruments::Instrument * GetInstrument(int id) const
Get the Instrument object.
Definition: Spacecraft.cpp:163
IO::SDK::Body::Spacecraft::Spacecraft::GetEphemerisCoverageWindow
IO::SDK::Time::Window< IO::SDK::Time::TDB > GetEphemerisCoverageWindow() const
Get the Ephemeris Coverage Window object.
Definition: Spacecraft.cpp:101
diff --git a/Docs/html/StateVector_8h_source.html b/Docs/html/StateVector_8h_source.html index 53f4f6a5..f3fd7fe2 100644 --- a/Docs/html/StateVector_8h_source.html +++ b/Docs/html/StateVector_8h_source.html @@ -182,7 +182,7 @@
IO::SDK::Frames::Frames
Frames base class.
Definition: Frames.h:26
IO::SDK::Math::Vector3D
Definition: Vector3D.h:17
IO::SDK::OrbitalParameters::OrbitalParameters
Orbital parameters.
Definition: OrbitalParameters.h:34
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector() const
Get the State Vector at epoch.
Definition: OrbitalParameters.cpp:124
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector() const
Get the State Vector at epoch.
Definition: OrbitalParameters.cpp:126
IO::SDK::OrbitalParameters::StateVector
State vector class.
Definition: StateVector.h:25
IO::SDK::OrbitalParameters::StateVector::operator==
bool operator==(const StateVector &other) const
Compare two state vectors.
Definition: StateVector.cpp:110
IO::SDK::OrbitalParameters::StateVector::operator=
StateVector & operator=(const StateVector &other)
Definition: StateVector.cpp:41
diff --git a/Docs/html/TLE_8h_source.html b/Docs/html/TLE_8h_source.html index 26dc8f8b..679bfd39 100644 --- a/Docs/html/TLE_8h_source.html +++ b/Docs/html/TLE_8h_source.html @@ -149,7 +149,7 @@
ConicOrbitalElements.h
IO::SDK::Math::Vector3D
Definition: Vector3D.h:17
IO::SDK::OrbitalParameters::OrbitalParameters
Orbital parameters.
Definition: OrbitalParameters.h:34
-
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector() const
Get the State Vector at epoch.
Definition: OrbitalParameters.cpp:124
+
IO::SDK::OrbitalParameters::OrbitalParameters::GetStateVector
virtual StateVector GetStateVector() const
Get the State Vector at epoch.
Definition: OrbitalParameters.cpp:126
IO::SDK::OrbitalParameters::OrbitalParameters::GetMeanAnomaly
virtual double GetMeanAnomaly() const =0
Get the Mean Anomaly.
IO::SDK::OrbitalParameters::StateVector
State vector class.
Definition: StateVector.h:25
IO::SDK::OrbitalParameters::TLE
Definition: TLE.h:19
diff --git a/Docs/html/TowardObjectAttitude_8h_source.html b/Docs/html/TowardObjectAttitude_8h_source.html index a9bebc8c..5276f81c 100644 --- a/Docs/html/TowardObjectAttitude_8h_source.html +++ b/Docs/html/TowardObjectAttitude_8h_source.html @@ -112,9 +112,9 @@
44 IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override;
45
46 public:
-
54 TowardObjectAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration, const IO::SDK::Body::Body &targetBody);
+
54 TowardObjectAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*>& engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration, const IO::SDK::Body::Body &targetBody);
55
-
64 TowardObjectAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration, const IO::SDK::Body::Body &targetBody);
+
64 TowardObjectAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*>& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration, const IO::SDK::Body::Body &targetBody);
65
73 bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override;
74 };
@@ -130,7 +130,7 @@
IO::SDK::Body::Body
Body class.
Definition: Body.h:38
IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude
Definition: TowardObjectAttitude.h:26
IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: TowardObjectAttitude.cpp:34
-
IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::TowardObjectAttitude
TowardObjectAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody)
Construct a new Toward Object Attitude object.
Definition: TowardObjectAttitude.cpp:13
+
IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::TowardObjectAttitude
TowardObjectAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody)
Construct a new Toward Object Attitude object.
Definition: TowardObjectAttitude.cpp:13
IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: TowardObjectAttitude.cpp:43
IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: TowardObjectAttitude.cpp:28
IO::SDK::Maneuvers::ManeuverBase
Maneuverbase class used by concrete maneuvers.
Definition: ManeuverBase.h:36
diff --git a/Docs/html/ZenithAttitude_8h_source.html b/Docs/html/ZenithAttitude_8h_source.html index 18d0a0b7..4604325e 100644 --- a/Docs/html/ZenithAttitude_8h_source.html +++ b/Docs/html/ZenithAttitude_8h_source.html @@ -112,9 +112,9 @@
44 IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override;
45
46 public:
-
53 ZenithAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration);
+
53 ZenithAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*>& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration);
54
-
62 ZenithAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*> engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration);
+
62 ZenithAttitude(const std::vector<IO::SDK::Body::Spacecraft::Engine*>& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration);
63
71 bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override;
72 };
@@ -128,7 +128,7 @@
Vector3D.h
IO::SDK::Maneuvers::Attitudes::ZenithAttitude
Definition: ZenithAttitude.h:26
IO::SDK::Maneuvers::Attitudes::ZenithAttitude::CanExecute
bool CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
Evaluate if maneuver can occurs.
Definition: ZenithAttitude.cpp:32
-
IO::SDK::Maneuvers::Attitudes::ZenithAttitude::ZenithAttitude
ZenithAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
Construct a new Zenith Attitude object.
Definition: ZenithAttitude.cpp:13
+
IO::SDK::Maneuvers::Attitudes::ZenithAttitude::ZenithAttitude
ZenithAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
Construct a new Zenith Attitude object.
Definition: ZenithAttitude.cpp:13
IO::SDK::Maneuvers::Attitudes::ZenithAttitude::Compute
void Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute impulsive maneuver.
Definition: ZenithAttitude.cpp:23
IO::SDK::Maneuvers::Attitudes::ZenithAttitude::ComputeOrientation
IO::SDK::OrbitalParameters::StateOrientation ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) override
Compute orientation.
Definition: ZenithAttitude.cpp:27
IO::SDK::Maneuvers::ManeuverBase
Maneuverbase class used by concrete maneuvers.
Definition: ManeuverBase.h:36
diff --git a/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft-members.html b/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft-members.html index 044ae147..4c5fb7b3 100644 --- a/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft-members.html @@ -114,7 +114,7 @@ GetId() constIO::SDK::Body::Body GetInstrument(int id) constIO::SDK::Body::Spacecraft::Spacecraft GetMass() const overrideIO::SDK::Body::Spacecraft::Spacecraftvirtual - GetMaximumOperatingMass()IO::SDK::Body::Spacecraft::Spacecraftinline + GetMaximumOperatingMass() constIO::SDK::Body::Spacecraft::Spacecraftinline GetMu() constIO::SDK::Body::Body GetName() constIO::SDK::Body::Body GetOrbitalParametersAtEpoch() constIO::SDK::Body::Body diff --git a/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html b/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html index 21528235..0eadc57f 100644 --- a/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html +++ b/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html @@ -189,8 +189,8 @@   const std::unique_ptr< IO::SDK::Frames::SpacecraftFrameFile > & GetFrame () const   -double GetMaximumOperatingMass () -  +double GetMaximumOperatingMass () const +  - Public Member Functions inherited from IO::SDK::Body::Body  Body (int id, const std::string &name, double mass)  Construct a new Body object. More...
@@ -1065,8 +1065,8 @@

-

◆ GetMaximumOperatingMass()

+ +

◆ GetMaximumOperatingMass()

@@ -1078,7 +1078,7 @@

double IO::SDK::Body::Spacecraft::Spacecraft::GetMaximumOperatingMass ( ) - + const diff --git a/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.js b/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.js index 9b2164ca..d8acd327 100644 --- a/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.js +++ b/Docs/html/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.js @@ -19,7 +19,7 @@ var classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft = [ "GetFueltank", "classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html#a347135bd0b7c9834754e0b5cf366f4de", null ], [ "GetInstrument", "classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html#afb07d602e067c059ac6ae3a573984fcb", null ], [ "GetMass", "classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html#ae7354800272662d52d64c5a1f2ade5c0", null ], - [ "GetMaximumOperatingMass", "classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html#aebe8482d25128fdb0e64466e68c84609", null ], + [ "GetMaximumOperatingMass", "classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html#ab83dd50751732be26d21cff147fcd548", null ], [ "GetOrientation", "classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html#ababce78d27520ce4fe4ee9a86ff5049b", null ], [ "GetOrientationsCoverageWindow", "classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html#a30b054da19d424c78fb2686f40f316d3", null ], [ "ReadEphemeris", "classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.html#ad061367c27a97a86d76d670b0bfdad02", null ], diff --git a/Docs/html/classIO_1_1SDK_1_1Coordinate-members.html b/Docs/html/classIO_1_1SDK_1_1Coordinate-members.html index 0afc03f2..d07ddc46 100644 --- a/Docs/html/classIO_1_1SDK_1_1Coordinate-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Coordinate-members.html @@ -91,7 +91,7 @@ - + @@ -100,7 +100,7 @@ - + diff --git a/Docs/html/classIO_1_1SDK_1_1Coordinate.html b/Docs/html/classIO_1_1SDK_1_1Coordinate.html index a247c39c..54e48372 100644 --- a/Docs/html/classIO_1_1SDK_1_1Coordinate.html +++ b/Docs/html/classIO_1_1SDK_1_1Coordinate.html @@ -95,9 +95,9 @@
Altitude()IO::SDK::Coordinatestatic
Colatitude()IO::SDK::Coordinatestatic
Coordinate(const std::string &name)IO::SDK::Coordinateexplicit
Coordinate(std::string name)IO::SDK::Coordinateexplicit
Declination()IO::SDK::Coordinatestatic
Latitude()IO::SDK::Coordinatestatic
Longitude()IO::SDK::Coordinatestatic
Range()IO::SDK::Coordinatestatic
RightAscension()IO::SDK::Coordinatestatic
ToCharArray() constIO::SDK::Coordinate
ToCoordinateType(const std::string &coordinateType)IO::SDK::Coordinatestatic
ToCoordinateType(const std::string &coordinateType)IO::SDK::Coordinatestatic
X()IO::SDK::Coordinatestatic
Y()IO::SDK::Coordinatestatic
Z()IO::SDK::Coordinatestatic
- - - + + + @@ -130,12 +130,12 @@ - - + +

Public Member Functions

 Coordinate (const std::string &name)
 Construct a new Coordinate object. More...
 
 Coordinate (std::string name)
 Construct a new Coordinate object. More...
 
 ~Coordinate ()=default
 
Coordinate & operator= (const Coordinate &other)
 
static Coordinate & Colatitude ()
 
static Coordinate ToCoordinateType (const std::string &coordinateType)
 
static Coordinate & ToCoordinateType (const std::string &coordinateType)
 

Constructor & Destructor Documentation

- -

◆ Coordinate()

+ +

◆ Coordinate()

@@ -146,7 +146,7 @@

IO::SDK::Coordinate::Coordinate ( - const std::string &  + std::string  name) @@ -440,8 +440,8 @@

-

◆ ToCoordinateType()

+ +

◆ ToCoordinateType()

@@ -450,7 +450,7 @@

- + diff --git a/Docs/html/classIO_1_1SDK_1_1Coordinate.js b/Docs/html/classIO_1_1SDK_1_1Coordinate.js index 5072758a..54d3fc4f 100644 --- a/Docs/html/classIO_1_1SDK_1_1Coordinate.js +++ b/Docs/html/classIO_1_1SDK_1_1Coordinate.js @@ -1,6 +1,6 @@ var classIO_1_1SDK_1_1Coordinate = [ - [ "Coordinate", "classIO_1_1SDK_1_1Coordinate.html#a14bc2970fed38a4ef4048cac18b7e716", null ], + [ "Coordinate", "classIO_1_1SDK_1_1Coordinate.html#ae1108a85782007065e647a88cad77365", null ], [ "~Coordinate", "classIO_1_1SDK_1_1Coordinate.html#a1d592a91467a7d574105e8e29e8b5172", null ], [ "operator=", "classIO_1_1SDK_1_1Coordinate.html#a48d76683e3f820e61293b3b300dd59ac", null ], [ "ToCharArray", "classIO_1_1SDK_1_1Coordinate.html#a5cdb9ede2c0a59dc0f37ea5a44a97a86", null ] diff --git a/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile-members.html b/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile-members.html index 0e396e35..2d3db307 100644 --- a/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile-members.html @@ -89,7 +89,7 @@

This is the complete list of members for IO::SDK::Frames::FrameFile, including all inherited members.

IO::SDK::Coordinate IO::SDK::Coordinate::ToCoordinateType IO::SDK::Coordinate & IO::SDK::Coordinate::ToCoordinateType ( const std::string &  coordinateType)
- + diff --git a/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile.html b/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile.html index a018c06b..d50cbaf7 100644 --- a/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile.html +++ b/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile.html @@ -118,8 +118,8 @@
FrameFile(const std::string &filePath, const std::string &name)IO::SDK::Frames::FrameFileprotected
FrameFile(const std::string &filePath, std::string name)IO::SDK::Frames::FrameFileprotected
GetName() constIO::SDK::Frames::FrameFile
m_fileExistsIO::SDK::Frames::FrameFileprotected
m_filePathIO::SDK::Frames::FrameFileprotected
- - + +

Protected Member Functions

 FrameFile (const std::string &filePath, const std::string &name)
 
 FrameFile (const std::string &filePath, std::string name)
 
@@ -135,8 +135,8 @@

Detailed Description

Frame file.

Constructor & Destructor Documentation

- -

◆ FrameFile()

+ +

◆ FrameFile()

@@ -153,7 +153,7 @@

- + diff --git a/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile.js b/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile.js index 447e701c..9cc4774c 100644 --- a/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile.js +++ b/Docs/html/classIO_1_1SDK_1_1Frames_1_1FrameFile.js @@ -1,6 +1,6 @@ var classIO_1_1SDK_1_1Frames_1_1FrameFile = [ - [ "FrameFile", "classIO_1_1SDK_1_1Frames_1_1FrameFile.html#a7671ea08db5c6c165d75ec5760c0bd23", null ], + [ "FrameFile", "classIO_1_1SDK_1_1Frames_1_1FrameFile.html#aa66f02e3afdcd901dafed6661c8a1b28", null ], [ "~FrameFile", "classIO_1_1SDK_1_1Frames_1_1FrameFile.html#a750a6ff9d670ffbbae82690f2d2208d4", null ], [ "GetName", "classIO_1_1SDK_1_1Frames_1_1FrameFile.html#a6fbe10b5ca7dc1dacea1b36c0c6336c3", null ], [ "m_fileExists", "classIO_1_1SDK_1_1Frames_1_1FrameFile.html#aee3f358a8ff43053e026d84c5c999181", null ], diff --git a/Docs/html/classIO_1_1SDK_1_1Frames_1_1InstrumentFrameFile-members.html b/Docs/html/classIO_1_1SDK_1_1Frames_1_1InstrumentFrameFile-members.html index 58e8082f..99d08271 100644 --- a/Docs/html/classIO_1_1SDK_1_1Frames_1_1InstrumentFrameFile-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Frames_1_1InstrumentFrameFile-members.html @@ -89,7 +89,7 @@

This is the complete list of members for IO::SDK::Frames::InstrumentFrameFile, including all inherited members.

Protected Attributes

const std::string & std::string  name 
- + diff --git a/Docs/html/classIO_1_1SDK_1_1Frames_1_1InstrumentFrameFile.html b/Docs/html/classIO_1_1SDK_1_1Frames_1_1InstrumentFrameFile.html index b534cf33..288c6956 100644 --- a/Docs/html/classIO_1_1SDK_1_1Frames_1_1InstrumentFrameFile.html +++ b/Docs/html/classIO_1_1SDK_1_1Frames_1_1InstrumentFrameFile.html @@ -118,8 +118,8 @@ - - + + diff --git a/Docs/html/classIO_1_1SDK_1_1Frames_1_1SiteFrameFile-members.html b/Docs/html/classIO_1_1SDK_1_1Frames_1_1SiteFrameFile-members.html index 513da40f..8dcd9d90 100644 --- a/Docs/html/classIO_1_1SDK_1_1Frames_1_1SiteFrameFile-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Frames_1_1SiteFrameFile-members.html @@ -89,7 +89,7 @@

This is the complete list of members for IO::SDK::Frames::SiteFrameFile, including all inherited members.

FrameFile(const std::string &filePath, const std::string &name)IO::SDK::Frames::FrameFileprotected
FrameFile(const std::string &filePath, std::string name)IO::SDK::Frames::FrameFileprotected
GetName() constIO::SDK::Frames::FrameFile
IO::SDK::Instruments::InstrumentIO::SDK::Frames::InstrumentFrameFilefriend
m_fileExistsIO::SDK::Frames::FrameFileprotected
 Get the frame name. More...
 
- Protected Member Functions inherited from IO::SDK::Frames::FrameFile
 FrameFile (const std::string &filePath, const std::string &name)
 
 FrameFile (const std::string &filePath, std::string name)
 
- Protected Attributes inherited from IO::SDK::Frames::FrameFile
const std::string m_filePath {}
 
- + diff --git a/Docs/html/classIO_1_1SDK_1_1Frames_1_1SiteFrameFile.html b/Docs/html/classIO_1_1SDK_1_1Frames_1_1SiteFrameFile.html index 7650c9cd..87bfe46f 100644 --- a/Docs/html/classIO_1_1SDK_1_1Frames_1_1SiteFrameFile.html +++ b/Docs/html/classIO_1_1SDK_1_1Frames_1_1SiteFrameFile.html @@ -119,8 +119,8 @@ - - + + diff --git a/Docs/html/classIO_1_1SDK_1_1Frames_1_1SpacecraftFrameFile-members.html b/Docs/html/classIO_1_1SDK_1_1Frames_1_1SpacecraftFrameFile-members.html index 6ded5326..072044ae 100644 --- a/Docs/html/classIO_1_1SDK_1_1Frames_1_1SpacecraftFrameFile-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Frames_1_1SpacecraftFrameFile-members.html @@ -89,7 +89,7 @@

This is the complete list of members for IO::SDK::Frames::SpacecraftFrameFile, including all inherited members.

FrameFile(const std::string &filePath, const std::string &name)IO::SDK::Frames::FrameFileprotected
FrameFile(const std::string &filePath, std::string name)IO::SDK::Frames::FrameFileprotected
GetName() constIO::SDK::Frames::FrameFile
m_fileExistsIO::SDK::Frames::FrameFileprotected
m_filePathIO::SDK::Frames::FrameFileprotected

Additional Inherited Members

- Protected Member Functions inherited from IO::SDK::Frames::FrameFile
 FrameFile (const std::string &filePath, const std::string &name)
 
 FrameFile (const std::string &filePath, std::string name)
 
- Protected Attributes inherited from IO::SDK::Frames::FrameFile
const std::string m_filePath {}
 
- + diff --git a/Docs/html/classIO_1_1SDK_1_1Frames_1_1SpacecraftFrameFile.html b/Docs/html/classIO_1_1SDK_1_1Frames_1_1SpacecraftFrameFile.html index 8713b693..740b10f8 100644 --- a/Docs/html/classIO_1_1SDK_1_1Frames_1_1SpacecraftFrameFile.html +++ b/Docs/html/classIO_1_1SDK_1_1Frames_1_1SpacecraftFrameFile.html @@ -124,8 +124,8 @@ - - + + diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude-members.html b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude-members.html index 5a81f54f..08f33933 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude-members.html @@ -117,8 +117,8 @@ - - + +
FrameFile(const std::string &filePath, const std::string &name)IO::SDK::Frames::FrameFileprotected
FrameFile(const std::string &filePath, std::string name)IO::SDK::Frames::FrameFileprotected
GetId() constIO::SDK::Frames::SpacecraftFrameFileinline
GetName() constIO::SDK::Frames::FrameFile
IO::SDK::Body::Spacecraft::SpacecraftIO::SDK::Frames::SpacecraftFrameFilefriend

Additional Inherited Members

- Protected Member Functions inherited from IO::SDK::Frames::FrameFile
 FrameFile (const std::string &filePath, const std::string &name)
 
 FrameFile (const std::string &filePath, std::string name)
 
- Protected Attributes inherited from IO::SDK::Frames::FrameFile
const std::string m_filePath {}
 
ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch)IO::SDK::Maneuvers::ManeuverBaseprotected
ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::ManeuverBaseprotected
ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::ManeuverBaseprotected
NadirAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::NadirAttitude
NadirAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::NadirAttitude
NadirAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::NadirAttitude
NadirAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::NadirAttitude
SetNextManeuver(IO::SDK::Maneuvers::ManeuverBase &maneuver)IO::SDK::Maneuvers::ManeuverBasevirtual
TryExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint)IO::SDK::Maneuvers::ManeuverBase

diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html index 20294904..8656e1ec 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html @@ -104,12 +104,12 @@ - - - - - - + + + + + + @@ -206,8 +206,8 @@

Public Member Functions

 NadirAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Nadir Attitude object. More...
 
 NadirAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Nadir Attitude object. More...
 
 NadirAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Nadir Attitude object. More...
 
 NadirAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Nadir Attitude object. More...
 
bool CanExecute (const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
 Evaluate if maneuver can occurs. More...
 
 

Constructor & Destructor Documentation

- -

◆ NadirAttitude() [1/2]

+ +

◆ NadirAttitude() [1/2]

@@ -215,7 +215,7 @@

IO::SDK::Maneuvers::Attitudes::NadirAttitude::NadirAttitude ( - const std::vector< IO::SDK::Body::Spacecraft::Engine * >  + const std::vector< IO::SDK::Body::Spacecraft::Engine * > &  engines, @@ -249,8 +249,8 @@

-

◆ NadirAttitude() [2/2]

+ +

◆ NadirAttitude() [2/2]

@@ -258,7 +258,7 @@

IO::SDK::Maneuvers::Attitudes::NadirAttitude::NadirAttitude ( - const std::vector< IO::SDK::Body::Spacecraft::Engine * >  + const std::vector< IO::SDK::Body::Spacecraft::Engine * > &  engines, diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.js b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.js index 74138ca9..d2e50e96 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.js +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.js @@ -1,7 +1,7 @@ var classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude = [ - [ "NadirAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html#a1c42b8b24041b935c7c39ff8713659da", null ], - [ "NadirAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html#af72bad35d416092ca326ca93906757c7", null ], + [ "NadirAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html#a19100017abcc10cbc88c768ad3d83c8c", null ], + [ "NadirAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html#aff17952207dcb51f47cc93fedb0b20fb", null ], [ "CanExecute", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html#a9f7b6b754fcf56017f44c1499a3decb1", null ], [ "Compute", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html#a4001fc23a9f67eb3be581b0322e5907c", null ], [ "ComputeOrientation", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude.html#ad6c8b02e0d98d55a3f047a67638261cd", null ] diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude-members.html b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude-members.html index aab83ee3..92edf435 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude-members.html @@ -117,8 +117,8 @@ ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch)IO::SDK::Maneuvers::ManeuverBaseprotected ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::ManeuverBaseprotected ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::ManeuverBaseprotected - ProgradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::ProgradeAttitude - ProgradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::ProgradeAttitude + ProgradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::ProgradeAttitude + ProgradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::ProgradeAttitude SetNextManeuver(IO::SDK::Maneuvers::ManeuverBase &maneuver)IO::SDK::Maneuvers::ManeuverBasevirtual TryExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint)IO::SDK::Maneuvers::ManeuverBase

diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html index 906c3efd..82b1e67e 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html @@ -104,12 +104,12 @@ - - - - - - + + + + + + @@ -206,8 +206,8 @@

Public Member Functions

 ProgradeAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Prograde Attitude object. More...
 
 ProgradeAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Prograde Attitude object. More...
 
 ProgradeAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Prograde Attitude object. More...
 
 ProgradeAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Prograde Attitude object. More...
 
bool CanExecute (const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
 Evaluate if maneuver can occurs. More...
 
 

Constructor & Destructor Documentation

- -

◆ ProgradeAttitude() [1/2]

+ +

◆ ProgradeAttitude() [1/2]

@@ -215,7 +215,7 @@

IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::ProgradeAttitude ( - const std::vector< IO::SDK::Body::Spacecraft::Engine * >  + const std::vector< IO::SDK::Body::Spacecraft::Engine * > &  engines, @@ -249,8 +249,8 @@

-

◆ ProgradeAttitude() [2/2]

+ +

◆ ProgradeAttitude() [2/2]

@@ -258,7 +258,7 @@

IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::ProgradeAttitude ( - const std::vector< IO::SDK::Body::Spacecraft::Engine * >  + const std::vector< IO::SDK::Body::Spacecraft::Engine * > &  engines, diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.js b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.js index 801b0a9b..c1b656f1 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.js +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.js @@ -1,7 +1,7 @@ var classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude = [ - [ "ProgradeAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html#a4befd3aa292dd8185e87c1f7b62f22c0", null ], - [ "ProgradeAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html#acfbcf91813954fb69de921837275049c", null ], + [ "ProgradeAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html#a73af1392368d15c48ee2f892eef72f34", null ], + [ "ProgradeAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html#ace2dd4a4221b2eb4cffae30ba6a4ee74", null ], [ "CanExecute", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html#acc05df379c165ce5052799888f9e3719", null ], [ "Compute", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html#a225c851079cdcaa986ba9eb715c2994c", null ], [ "ComputeOrientation", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.html#a794ab49935a4feced62692674ea8109d", null ] diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude-members.html b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude-members.html index 6da85077..ff704a06 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude-members.html @@ -117,8 +117,8 @@ ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch)IO::SDK::Maneuvers::ManeuverBaseprotected ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::ManeuverBaseprotected ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::ManeuverBaseprotected - RetrogradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude - RetrogradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude + RetrogradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude + RetrogradeAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude SetNextManeuver(IO::SDK::Maneuvers::ManeuverBase &maneuver)IO::SDK::Maneuvers::ManeuverBasevirtual TryExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint)IO::SDK::Maneuvers::ManeuverBase

diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html index 49b8a98f..a8cbe53e 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html @@ -104,12 +104,12 @@ - - - - - - + + + + + + @@ -206,8 +206,8 @@

Public Member Functions

 RetrogradeAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Retrograde Attitude object. More...
 
 RetrogradeAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Retrograde Attitude object. More...
 
 RetrogradeAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Retrograde Attitude object. More...
 
 RetrogradeAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Retrograde Attitude object. More...
 
bool CanExecute (const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
 Evaluate if maneuver can occurs. More...
 
 

Constructor & Destructor Documentation

- -

◆ RetrogradeAttitude() [1/2]

+ +

◆ RetrogradeAttitude() [1/2]

@@ -215,7 +215,7 @@

IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::RetrogradeAttitude ( - const std::vector< IO::SDK::Body::Spacecraft::Engine * >  + const std::vector< IO::SDK::Body::Spacecraft::Engine * > &  engines, @@ -249,8 +249,8 @@

-

◆ RetrogradeAttitude() [2/2]

+ +

◆ RetrogradeAttitude() [2/2]

@@ -258,7 +258,7 @@

IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::RetrogradeAttitude ( - const std::vector< IO::SDK::Body::Spacecraft::Engine * >  + const std::vector< IO::SDK::Body::Spacecraft::Engine * > &  engines, diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.js b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.js index 8213b539..e8ed4135 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.js +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.js @@ -1,7 +1,7 @@ var classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude = [ - [ "RetrogradeAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html#a3867ab497cd0e694917d20e9d9a43334", null ], - [ "RetrogradeAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html#add864c9248cf817e195e287acd8ed534", null ], + [ "RetrogradeAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html#a1c0f94622fa6b2c3641afe8a51da367b", null ], + [ "RetrogradeAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html#a9e29a9c3846c15e59c11be42a47eb004", null ], [ "CanExecute", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html#ace8726c7e00edf44bb790be5050a7f24", null ], [ "Compute", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html#ad96bb05dd539d40d01139b9c06fb972d", null ], [ "ComputeOrientation", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.html#a8f938d701ccc27bd757bd1017e3561c7", null ] diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude-members.html b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude-members.html index 9bd20daa..21830e35 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude-members.html @@ -118,8 +118,8 @@ ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::ManeuverBaseprotected ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::ManeuverBaseprotected SetNextManeuver(IO::SDK::Maneuvers::ManeuverBase &maneuver)IO::SDK::Maneuvers::ManeuverBasevirtual - TowardObjectAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody)IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude - TowardObjectAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody)IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude + TowardObjectAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody)IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude + TowardObjectAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody)IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude TryExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint)IO::SDK::Maneuvers::ManeuverBase

diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html index 11af911c..8919e672 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html @@ -104,12 +104,12 @@ - - - - - - + + + + + + @@ -206,8 +206,8 @@

Public Member Functions

 TowardObjectAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody)
 Construct a new Toward Object Attitude object. More...
 
 TowardObjectAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody)
 Construct a new Toward Object Attitude object. More...
 
 TowardObjectAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody)
 Construct a new Toward Object Attitude object. More...
 
 TowardObjectAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody)
 Construct a new Toward Object Attitude object. More...
 
bool CanExecute (const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
 Evaluate if maneuver can occurs. More...
 
 

Constructor & Destructor Documentation

- -

◆ TowardObjectAttitude() [1/2]

+ +

◆ TowardObjectAttitude() [1/2]

@@ -215,7 +215,7 @@

IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::TowardObjectAttitude ( - const std::vector< IO::SDK::Body::Spacecraft::Engine * >  + const std::vector< IO::SDK::Body::Spacecraft::Engine * > &  engines, @@ -256,8 +256,8 @@

-

◆ TowardObjectAttitude() [2/2]

+ +

◆ TowardObjectAttitude() [2/2]

@@ -265,7 +265,7 @@

IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::TowardObjectAttitude ( - const std::vector< IO::SDK::Body::Spacecraft::Engine * >  + const std::vector< IO::SDK::Body::Spacecraft::Engine * > &  engines, diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.js b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.js index 40b780a8..c84117e9 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.js +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.js @@ -1,7 +1,7 @@ var classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude = [ - [ "TowardObjectAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html#a4f54adecfccb8b73e08a0bf8aef7dccb", null ], - [ "TowardObjectAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html#aa55d17808cf7bdfef7ae703d985171d1", null ], + [ "TowardObjectAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html#a6a1d2837006c792f1416441e4311c3ce", null ], + [ "TowardObjectAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html#a5688038cc3a244c76b0bb8f53bd43b2b", null ], [ "CanExecute", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html#a8d3620611d4b1983dfc2a15fbb9b1128", null ], [ "Compute", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html#aa434bb37713a5a45791625ecff25fe90", null ], [ "ComputeOrientation", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.html#a2296926c7cc97c3d118181b802f3720c", null ] diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude-members.html b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude-members.html index c1422671..01eff060 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude-members.html @@ -119,8 +119,8 @@ ManeuverBase(std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::ManeuverBaseprotected SetNextManeuver(IO::SDK::Maneuvers::ManeuverBase &maneuver)IO::SDK::Maneuvers::ManeuverBasevirtual TryExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint)IO::SDK::Maneuvers::ManeuverBase - ZenithAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::ZenithAttitude - ZenithAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::ZenithAttitude + ZenithAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::ZenithAttitude + ZenithAttitude(const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)IO::SDK::Maneuvers::Attitudes::ZenithAttitude

diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html index 29e67333..9014b544 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html @@ -104,12 +104,12 @@ - - - - - - + + + + + + @@ -206,8 +206,8 @@

Public Member Functions

 ZenithAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Zenith Attitude object. More...
 
 ZenithAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Zenith Attitude object. More...
 
 ZenithAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Zenith Attitude object. More...
 
 ZenithAttitude (const std::vector< IO::SDK::Body::Spacecraft::Engine * > &engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration)
 Construct a new Zenith Attitude object. More...
 
bool CanExecute (const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) override
 Evaluate if maneuver can occurs. More...
 
 

Constructor & Destructor Documentation

- -

◆ ZenithAttitude() [1/2]

+ +

◆ ZenithAttitude() [1/2]

@@ -215,7 +215,7 @@

IO::SDK::Maneuvers::Attitudes::ZenithAttitude::ZenithAttitude ( - const std::vector< IO::SDK::Body::Spacecraft::Engine * >  + const std::vector< IO::SDK::Body::Spacecraft::Engine * > &  engines, @@ -249,8 +249,8 @@

-

◆ ZenithAttitude() [2/2]

+ +

◆ ZenithAttitude() [2/2]

@@ -258,7 +258,7 @@

IO::SDK::Maneuvers::Attitudes::ZenithAttitude::ZenithAttitude ( - const std::vector< IO::SDK::Body::Spacecraft::Engine * >  + const std::vector< IO::SDK::Body::Spacecraft::Engine * > &  engines, diff --git a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.js b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.js index ed248e2a..0a4b0299 100644 --- a/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.js +++ b/Docs/html/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.js @@ -1,7 +1,7 @@ var classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude = [ - [ "ZenithAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html#a3dfe74492c2bed032f37ac4d02e153be", null ], - [ "ZenithAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html#a561ebd27bde3dd63d1e782ca35548fb6", null ], + [ "ZenithAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html#a75359142c87e83ac94578e3b92242239", null ], + [ "ZenithAttitude", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html#a1fd89c8b1e1a85f1b6bad1cdcd72410e", null ], [ "CanExecute", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html#a02199451b76c086541d3a99f5032ed84", null ], [ "Compute", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html#abcc5ebba2edb760cc3d08e8dbc6a9e60", null ], [ "ComputeOrientation", "classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.html#adb59be8151c3be823650ed5a0f1d16f4", null ] diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1ConicOrbitalElements-members.html b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1ConicOrbitalElements-members.html index de38c939..306a08a1 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1ConicOrbitalElements-members.html +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1ConicOrbitalElements-members.html @@ -136,7 +136,7 @@ m_centerOfMotionIO::SDK::OrbitalParameters::OrbitalParametersprotected m_epochIO::SDK::OrbitalParameters::OrbitalParametersprotected m_frameIO::SDK::OrbitalParameters::OrbitalParametersprotected - OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)IO::SDK::OrbitalParameters::OrbitalParameters + OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame)IO::SDK::OrbitalParameters::OrbitalParameters ~ConicOrbitalElements() override=defaultIO::SDK::OrbitalParameters::ConicOrbitalElements ~OrbitalParameters()=defaultIO::SDK::OrbitalParameters::OrbitalParametersvirtual

diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1ConicOrbitalElements.html b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1ConicOrbitalElements.html index b9283ad5..7abe925b 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1ConicOrbitalElements.html +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1ConicOrbitalElements.html @@ -166,9 +166,9 @@  Get the True Anomaly. More...
  - Public Member Functions inherited from IO::SDK::OrbitalParameters::OrbitalParameters - OrbitalParameters (const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame) - Construct a new Orbital Parameters object. More...
-  + OrbitalParameters (const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame) + Construct a new Orbital Parameters object. More...
+  virtual ~OrbitalParameters ()=default   const std::shared_ptr< IO::SDK::Body::CelestialBody > & GetCenterOfMotion () const diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1EquinoctialElements-members.html b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1EquinoctialElements-members.html index 5e4d4dab..1a54d0d2 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1EquinoctialElements-members.html +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1EquinoctialElements-members.html @@ -142,7 +142,7 @@ m_centerOfMotionIO::SDK::OrbitalParameters::OrbitalParametersprotected m_epochIO::SDK::OrbitalParameters::OrbitalParametersprotected m_frameIO::SDK::OrbitalParameters::OrbitalParametersprotected - OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)IO::SDK::OrbitalParameters::OrbitalParameters + OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame)IO::SDK::OrbitalParameters::OrbitalParameters ~OrbitalParameters()=defaultIO::SDK::OrbitalParameters::OrbitalParametersvirtual

diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1EquinoctialElements.html b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1EquinoctialElements.html index ff1c83e8..15ca71a9 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1EquinoctialElements.html +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1EquinoctialElements.html @@ -174,9 +174,9 @@  Get the Mean Anomaly. More...
  - Public Member Functions inherited from IO::SDK::OrbitalParameters::OrbitalParameters - OrbitalParameters (const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame) - Construct a new Orbital Parameters object. More...
-  + OrbitalParameters (const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame) + Construct a new Orbital Parameters object. More...
+  virtual ~OrbitalParameters ()=default   const std::shared_ptr< IO::SDK::Body::CelestialBody > & GetCenterOfMotion () const diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters-members.html b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters-members.html index c7995229..d121a141 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters-members.html +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters-members.html @@ -129,7 +129,7 @@ m_centerOfMotionIO::SDK::OrbitalParameters::OrbitalParametersprotected m_epochIO::SDK::OrbitalParameters::OrbitalParametersprotected m_frameIO::SDK::OrbitalParameters::OrbitalParametersprotected - OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)IO::SDK::OrbitalParameters::OrbitalParameters + OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame)IO::SDK::OrbitalParameters::OrbitalParameters ~OrbitalParameters()=defaultIO::SDK::OrbitalParameters::OrbitalParametersvirtual

diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.html b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.html index 32279a5a..93e1cb76 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.html +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.html @@ -110,9 +110,9 @@ - - - + + + @@ -239,8 +239,8 @@

Detailed Description

Orbital parameters.

Constructor & Destructor Documentation

- -

◆ OrbitalParameters()

+ +

◆ OrbitalParameters()

@@ -254,13 +254,13 @@

- + - + diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.js b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.js index a72422da..71ed3763 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.js +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.js @@ -1,6 +1,6 @@ var classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters = [ - [ "OrbitalParameters", "classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.html#aa2ad5e93197a2465c3cf50b8065f6d61", null ], + [ "OrbitalParameters", "classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.html#a2e151aad0e34a4bc0918f93ec536ea58", null ], [ "~OrbitalParameters", "classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.html#a4c24cb357f03afe566885b46b86797c0", null ], [ "GetApogeeVector", "classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.html#a6db13919245724695465b77c60438492", null ], [ "GetAscendingNodeVector", "classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters.html#acaadaa0b6f59cf7589a36e809a4ca86e", null ], diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector-members.html b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector-members.html index 6089559a..583f94d7 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector-members.html +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector-members.html @@ -134,7 +134,7 @@ - + diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector.html b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector.html index 0bed94ea..1fe40f24 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector.html +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector.html @@ -173,9 +173,9 @@ - - - + + + diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1TLE-members.html b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1TLE-members.html index 6ea06375..8a10a150 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1TLE-members.html +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1TLE-members.html @@ -134,7 +134,7 @@ - + diff --git a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1TLE.html b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1TLE.html index 03ba05fd..cdd74618 100644 --- a/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1TLE.html +++ b/Docs/html/classIO_1_1SDK_1_1OrbitalParameters_1_1TLE.html @@ -156,9 +156,9 @@ - - - + + + diff --git a/Docs/html/classIO_1_1SDK_1_1Scenario-members.html b/Docs/html/classIO_1_1SDK_1_1Scenario-members.html index a5416bb1..2e3bc615 100644 --- a/Docs/html/classIO_1_1SDK_1_1Scenario-members.html +++ b/Docs/html/classIO_1_1SDK_1_1Scenario-members.html @@ -89,24 +89,17 @@

This is the complete list of members for IO::SDK::Scenario, including all inherited members.

Public Member Functions

 OrbitalParameters (const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)
 Construct a new Orbital Parameters object. More...
 
 OrbitalParameters (const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame)
 Construct a new Orbital Parameters object. More...
 
virtual ~OrbitalParameters ()=default
 
const std::shared_ptr< IO::SDK::Body::CelestialBody > & GetCenterOfMotion () const
const IO::SDK::Time::TDB & IO::SDK::Time::TDB  epoch,
const IO::SDK::Frames::Frames & IO::SDK::Frames::Frames  frame 
m_frameIO::SDK::OrbitalParameters::OrbitalParametersprotected
operator=(const StateVector &other)IO::SDK::OrbitalParameters::StateVector
operator==(const StateVector &other) constIO::SDK::OrbitalParameters::StateVector
OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)IO::SDK::OrbitalParameters::OrbitalParameters
OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame)IO::SDK::OrbitalParameters::OrbitalParameters
StateVector(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Math::Vector3D &position, const IO::SDK::Math::Vector3D &velocity, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)IO::SDK::OrbitalParameters::StateVector
StateVector(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, double spiceState[6], const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)IO::SDK::OrbitalParameters::StateVector
StateVector(const StateVector &v)IO::SDK::OrbitalParameters::StateVector
 Convert state vector to body fixed frame. More...
 
- Public Member Functions inherited from IO::SDK::OrbitalParameters::OrbitalParameters
 OrbitalParameters (const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)
 Construct a new Orbital Parameters object. More...
 
 OrbitalParameters (const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame)
 Construct a new Orbital Parameters object. More...
 
virtual ~OrbitalParameters ()=default
 
const std::shared_ptr< IO::SDK::Body::CelestialBody > & GetCenterOfMotion () const
m_centerOfMotionIO::SDK::OrbitalParameters::OrbitalParametersprotected
m_epochIO::SDK::OrbitalParameters::OrbitalParametersprotected
m_frameIO::SDK::OrbitalParameters::OrbitalParametersprotected
OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)IO::SDK::OrbitalParameters::OrbitalParameters
OrbitalParameters(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame)IO::SDK::OrbitalParameters::OrbitalParameters
TLE(const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfmotion, std::string lines[3])IO::SDK::OrbitalParameters::TLE
~OrbitalParameters()=defaultIO::SDK::OrbitalParameters::OrbitalParametersvirtual
~TLE() override=defaultIO::SDK::OrbitalParameters::TLE
 Get the Mean Anomaly. More...
 
- Public Member Functions inherited from IO::SDK::OrbitalParameters::OrbitalParameters
 OrbitalParameters (const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame)
 Construct a new Orbital Parameters object. More...
 
 OrbitalParameters (const std::shared_ptr< IO::SDK::Body::CelestialBody > &centerOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame)
 Construct a new Orbital Parameters object. More...
 
virtual ~OrbitalParameters ()=default
 
const std::shared_ptr< IO::SDK::Body::CelestialBody > & GetCenterOfMotion () const
- - - - - - - - - - - - - - - - - - + + + + + + + + + + +
AddBodyVisibilityConstraint(IO::SDK::Constraints::Parameters::BodyVisibilityFromSiteParameters *bodyVisibilityParameters)IO::SDK::Scenario
AddCelestialBody(const IO::SDK::Body::CelestialBody &celestialBody)IO::SDK::Scenario
AddDayConstraint(IO::SDK::Constraints::Parameters::ByDayParameters *byDayParameters)IO::SDK::Scenario
AddDistanceConstraint(Constraints::Parameters::DistanceParameters *distanceParameters)IO::SDK::Scenario
AddInFieldOfViewConstraint(IO::SDK::Constraints::Parameters::InFieldOfViewParameters *inFieldOfViewParameters)IO::SDK::Scenario
AddLaunchConstraint(IO::SDK::Constraints::Parameters::LaunchParameters *launchParameters)IO::SDK::Scenario
AddNightConstraint(IO::SDK::Constraints::Parameters::ByNightParameters *byNightParameters)IO::SDK::Scenario
AddOccultationConstraint(IO::SDK::Constraints::Parameters::OccultationParameters *occultationParameters)IO::SDK::Scenario
AddSite(const IO::SDK::Sites::Site &site)IO::SDK::Scenario
AttachSpacecraft(const IO::SDK::Body::Spacecraft::Spacecraft &spacecraft)IO::SDK::Scenario
Execute()IO::SDK::Scenario
GetCelestialBodies()IO::SDK::Scenarioinline
GetName() constIO::SDK::Scenarioinline
GetPropagator()IO::SDK::Scenarioinline
GetSites()IO::SDK::Scenarioinline
GetSpacecraft()IO::SDK::Scenarioinline
GetWindow() constIO::SDK::Scenarioinline
Scenario(std::string name, const IO::SDK::Time::Window< IO::SDK::Time::UTC > &windows)IO::SDK::Scenario
AddCelestialBody(const IO::SDK::Body::CelestialBody &celestialBody)IO::SDK::Scenario
AddSite(const IO::SDK::Sites::Site &site)IO::SDK::Scenario
AttachSpacecraft(const IO::SDK::Body::Spacecraft::Spacecraft &spacecraft)IO::SDK::Scenario
Execute()IO::SDK::Scenario
GetCelestialBodies()IO::SDK::Scenarioinline
GetName() constIO::SDK::Scenarioinline
GetPropagator()IO::SDK::Scenarioinline
GetSites()IO::SDK::Scenarioinline
GetSpacecraft()IO::SDK::Scenarioinline
GetWindow() constIO::SDK::Scenarioinline
Scenario(std::string name, const IO::SDK::Time::Window< IO::SDK::Time::UTC > &windows)IO::SDK::Scenario

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Member Function Documentation

- -

◆ AddBodyVisibilityConstraint()

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void IO::SDK::Scenario::AddBodyVisibilityConstraint (IO::SDK::Constraints::Parameters::BodyVisibilityFromSiteParameters * bodyVisibilityParameters)
-
-

Add a body visibility constraint

Parameters
- - -
bodyVisibilityParameters
-
-
- -
-

◆ AddCelestialBody()

@@ -207,150 +169,6 @@

-

◆ AddDayConstraint()

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void IO::SDK::Scenario::AddDayConstraint (IO::SDK::Constraints::Parameters::ByDayParameters * byDayParameters)
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Add a day constraint

Parameters
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byDayParameters
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◆ AddDistanceConstraint()

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void IO::SDK::Scenario::AddDistanceConstraint (Constraints::Parameters::DistanceParameters * distanceParameters)
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Add a distance constraint

Parameters
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distanceParameters
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◆ AddInFieldOfViewConstraint()

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void IO::SDK::Scenario::AddInFieldOfViewConstraint (IO::SDK::Constraints::Parameters::InFieldOfViewParameters * inFieldOfViewParameters)
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Add a field of view constraint

Parameters
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inFieldOfViewParameters
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◆ AddLaunchConstraint()

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void IO::SDK::Scenario::AddLaunchConstraint (IO::SDK::Constraints::Parameters::LaunchParameters * launchParameters)
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Add launch constraint

Parameters
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launchParameters
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◆ AddNightConstraint()

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void IO::SDK::Scenario::AddNightConstraint (IO::SDK::Constraints::Parameters::ByNightParameters * byNightParameters)
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Add a night constraint

Parameters
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byNightParameters
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◆ AddOccultationConstraint()

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void IO::SDK::Scenario::AddOccultationConstraint (IO::SDK::Constraints::Parameters::OccultationParameters * occultationParameters)
-
-

Add an occultation constraint

Parameters
- - -
occultationParameters
-
-
-
@@ -415,7 +233,7 @@

-

Execute scenario, propagate spacecrafts, simulate maneuvers, evaluate constraints

+

Execute scenario

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- a -

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- a -

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- o -

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- p -

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- n -

  • nadirAttitudes : IO::SDK::API::DTO::SpacecraftDTO
  • Name : IO::SDK::API::DTO::CelestialBodyDTO
    • -
  • name : IO::SDK::API::DTO::EngineDTO, IO::SDK::API::DTO::InstrumentDTO, IO::SDK::API::DTO::PayloadDTO
    • -
  • Name : IO::SDK::API::DTO::ScenarioDTO
    • +
  • name : IO::SDK::API::DTO::EngineDTO, IO::SDK::API::DTO::InstrumentDTO, IO::SDK::API::DTO::PayloadDTO
    • +
  • Name : IO::SDK::API::DTO::ScenarioDTO
  • name : IO::SDK::API::DTO::SiteDTO, IO::SDK::API::DTO::SpacecraftDTO
  • nonInertialAzimuth : IO::SDK::API::DTO::LaunchDTO
  • nonInertialInsertionVelocity : IO::SDK::API::DTO::LaunchDTO
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    - s -

      -
    • serialNumber : IO::SDK::API::DTO::EngineDTO, IO::SDK::API::DTO::FuelTankDTO, IO::SDK::API::DTO::PayloadDTO
      • +
    • serialNumber : IO::SDK::API::DTO::EngineDTO, IO::SDK::API::DTO::FuelTankDTO, IO::SDK::API::DTO::PayloadDTO
    • shape : IO::SDK::API::DTO::InstrumentDTO
    • Sites : IO::SDK::API::DTO::ScenarioDTO
    • Spacecraft : IO::SDK::API::DTO::ScenarioDTO
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      - z -

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b/Docs/html/search/variables_b.js @@ -1,8 +1,8 @@ var searchData= [ ['nadirattitudes_0',['nadirAttitudes',['../structIO_1_1SDK_1_1API_1_1DTO_1_1SpacecraftDTO.html#a0a22f82f050fa489da9d3b28b89fbc21',1,'IO::SDK::API::DTO::SpacecraftDTO']]], - ['name_1',['name',['../structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#a8eba4c4ea41e59883a38b5b31fc0c1cd',1,'IO::SDK::API::DTO::EngineDTO::name()'],['../structIO_1_1SDK_1_1API_1_1DTO_1_1InstrumentDTO.html#ae1085834008351e68b8c291e192ee64d',1,'IO::SDK::API::DTO::InstrumentDTO::name()'],['../structIO_1_1SDK_1_1API_1_1DTO_1_1PayloadDTO.html#a12cf53527bd7a399ea89f515df58d517',1,'IO::SDK::API::DTO::PayloadDTO::name()'],['../structIO_1_1SDK_1_1API_1_1DTO_1_1SiteDTO.html#aff19f9ee62d2d1d3b306626c3585cf6a',1,'IO::SDK::API::DTO::SiteDTO::name()'],['../structIO_1_1SDK_1_1API_1_1DTO_1_1SpacecraftDTO.html#a1feb00c8c91a2af0c47591e572351b79',1,'IO::SDK::API::DTO::SpacecraftDTO::name()']]], - ['name_2',['Name',['../structIO_1_1SDK_1_1API_1_1DTO_1_1CelestialBodyDTO.html#ac58bd7effed87fb64a593b795a357a03',1,'IO::SDK::API::DTO::CelestialBodyDTO::Name()'],['../structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html#a46fecef09b2136f0d48b606cd0026430',1,'IO::SDK::API::DTO::ScenarioDTO::Name()']]], + ['name_1',['Name',['../structIO_1_1SDK_1_1API_1_1DTO_1_1CelestialBodyDTO.html#ac58bd7effed87fb64a593b795a357a03',1,'IO::SDK::API::DTO::CelestialBodyDTO::Name()'],['../structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html#a19b9d3b85ddcc93df6029ea267ab1a85',1,'IO::SDK::API::DTO::ScenarioDTO::Name()']]], + ['name_2',['name',['../structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#afba82457c3dba1f96881de6c7f96c6fc',1,'IO::SDK::API::DTO::EngineDTO::name()'],['../structIO_1_1SDK_1_1API_1_1DTO_1_1InstrumentDTO.html#ae1085834008351e68b8c291e192ee64d',1,'IO::SDK::API::DTO::InstrumentDTO::name()'],['../structIO_1_1SDK_1_1API_1_1DTO_1_1PayloadDTO.html#a12cf53527bd7a399ea89f515df58d517',1,'IO::SDK::API::DTO::PayloadDTO::name()'],['../structIO_1_1SDK_1_1API_1_1DTO_1_1SiteDTO.html#aff19f9ee62d2d1d3b306626c3585cf6a',1,'IO::SDK::API::DTO::SiteDTO::name()'],['../structIO_1_1SDK_1_1API_1_1DTO_1_1SpacecraftDTO.html#a1feb00c8c91a2af0c47591e572351b79',1,'IO::SDK::API::DTO::SpacecraftDTO::name()']]], ['nauticaltwilight_3',['NauticalTwilight',['../namespaceIO_1_1SDK_1_1Constants.html#a934c3fc0b60243bb14a32f797ec41329',1,'IO::SDK::Constants']]], ['nodedetectionaccuraccy_4',['NodeDetectionAccuraccy',['../namespaceIO_1_1SDK_1_1Parameters.html#afb6663fa378276d38946b2183ba2fc5f',1,'IO::SDK::Parameters']]], ['noninertialazimuth_5',['nonInertialAzimuth',['../structIO_1_1SDK_1_1API_1_1DTO_1_1LaunchDTO.html#a211ca52c4538c98461138364414c8969',1,'IO::SDK::API::DTO::LaunchDTO']]], diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO-members.html b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO-members.html index a583f9b4..ae1bbe8e 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO-members.html +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO-members.html @@ -89,12 +89,12 @@

      This is the complete list of members for IO::SDK::API::DTO::EngineDTO, including all inherited members.

      - - + + - - + +
      fuelflowIO::SDK::API::DTO::EngineDTO
      fuelTankSerialNumberIO::SDK::API::DTO::EngineDTO
      fuelFlowIO::SDK::API::DTO::EngineDTO
      fuelTankSerialNumberIO::SDK::API::DTO::EngineDTO
      idIO::SDK::API::DTO::EngineDTO
      ispIO::SDK::API::DTO::EngineDTO
      nameIO::SDK::API::DTO::EngineDTO
      serialNumberIO::SDK::API::DTO::EngineDTO
      nameIO::SDK::API::DTO::EngineDTO
      serialNumberIO::SDK::API::DTO::EngineDTO

diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html index 1a99b92f..62cf8132 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html @@ -96,40 +96,40 @@ Public Attributes

int id   -char * serialNumber -  -char * fuelTankSerialNumber -  -char * name -  +const char * serialNumber +  +const char * fuelTankSerialNumber +  +const char * name +  double isp   -double fuelflow -  +double fuelFlow + 

Member Data Documentation

- -

◆ fuelflow

+ +

◆ fuelFlow

- +
double IO::SDK::API::DTO::EngineDTO::fuelflowdouble IO::SDK::API::DTO::EngineDTO::fuelFlow
- -

◆ fuelTankSerialNumber

+ +

◆ fuelTankSerialNumber

- +
char* IO::SDK::API::DTO::EngineDTO::fuelTankSerialNumberconst char* IO::SDK::API::DTO::EngineDTO::fuelTankSerialNumber
@@ -164,28 +164,28 @@

-

◆ name

+ +

◆ name

- +
char* IO::SDK::API::DTO::EngineDTO::nameconst char* IO::SDK::API::DTO::EngineDTO::name
- -

◆ serialNumber

+ +

◆ serialNumber

- +
char* IO::SDK::API::DTO::EngineDTO::serialNumberconst char* IO::SDK::API::DTO::EngineDTO::serialNumber
diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.js b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.js index c53b06f3..d575d1bc 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.js +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.js @@ -1,9 +1,9 @@ var structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO = [ - [ "fuelflow", "structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#a9a295704e9d53487bbbb3d11fc5e99e8", null ], - [ "fuelTankSerialNumber", "structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#a57fb452f92b221d0628df58fcec099dd", null ], + [ "fuelFlow", "structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#acb4c6108c1622e33f4b016ac6e933fe6", null ], + [ "fuelTankSerialNumber", "structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#ae1586be547c6c629ef9fffa48ce3eb3e", null ], [ "id", "structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#ae946e724e129f39d66841a6c60fb357f", null ], [ "isp", "structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#a0ff30313e1775ad5bfcf6c290597bb83", null ], - [ "name", "structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#a8eba4c4ea41e59883a38b5b31fc0c1cd", null ], - [ "serialNumber", "structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#a37aaff67723471afe0b424b1c5f45b62", null ] + [ "name", "structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#afba82457c3dba1f96881de6c7f96c6fc", null ], + [ "serialNumber", "structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO.html#aaaef37ff022681b8c013aabc22cf6bd3", null ] ]; \ No newline at end of file diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO-members.html b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO-members.html index 61062fac..472080f6 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO-members.html +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO-members.html @@ -92,7 +92,7 @@ capacityIO::SDK::API::DTO::FuelTankDTO idIO::SDK::API::DTO::FuelTankDTO quantityIO::SDK::API::DTO::FuelTankDTO - serialNumberIO::SDK::API::DTO::FuelTankDTO + serialNumberIO::SDK::API::DTO::FuelTankDTO
diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.html b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.html index 6f60abae..d22f7daf 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.html +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.html @@ -96,8 +96,8 @@ Public Attributes

int id   -char * serialNumber -  +const char * serialNumber +  double capacity   double quantity @@ -146,14 +146,14 @@

-

◆ serialNumber

+ +

◆ serialNumber

- +
char* IO::SDK::API::DTO::FuelTankDTO::serialNumberconst char* IO::SDK::API::DTO::FuelTankDTO::serialNumber
diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.js b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.js index 73d9249d..a3c52bae 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.js +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.js @@ -3,5 +3,5 @@ var structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO = [ "capacity", "structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.html#aa8d92790c4185a373b2c013a2bb816ed", null ], [ "id", "structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.html#ad511fe1e6898cc0280b0069f1f44207e", null ], [ "quantity", "structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.html#a2e18763910cc002dfaccd86b1f23ef2e", null ], - [ "serialNumber", "structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.html#ad8aa5e4becba2f0767fa310849b8f1a1", null ] + [ "serialNumber", "structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.html#a52f3d0b45205f9b3e84f0bce316abe91", null ] ]; \ No newline at end of file diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO-members.html b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO-members.html index 49f0b602..50471be7 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO-members.html +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO-members.html @@ -92,7 +92,7 @@ attitudeHoldDurationIO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO attitudeWindowIO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO deltaVIO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO - enginesIO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO + enginesIO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO FuelBurnedIO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO maneuverOrderIO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO maneuverWindowIO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html index 2c71240f..a4de9e95 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html @@ -96,8 +96,8 @@ Public Attributes

int maneuverOrder {-1}   -char * engines [5] {} -  +const char * engines [5] {} +  double attitudeHoldDuration {0.0}   double minimumEpoch {0.0} @@ -158,14 +158,14 @@

-

◆ engines

+ +

◆ engines

- +
char* IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO::engines[5] {}const char* IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO::engines[5] {}
diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.js b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.js index a606ea91..6b888ff1 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.js +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.js @@ -3,7 +3,7 @@ var structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO = [ "attitudeHoldDuration", "structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html#ae949350a0a86deccbc35378e75a73e80", null ], [ "attitudeWindow", "structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html#a7695f7621ce2077a11e4f0c2b87a859d", null ], [ "deltaV", "structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html#ac08eaceb27e03b4add66c7c4d531ce86", null ], - [ "engines", "structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html#ac92b335a51002a99f037eaf11fe0cf1c", null ], + [ "engines", "structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html#ac68a3c6f143c4e2468ddeb1d6d091e99", null ], [ "FuelBurned", "structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html#a3e3483a71116f130eb080c7e7819905f", null ], [ "maneuverOrder", "structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html#a8c9d63e641f8ec865cc7c8e7369b0f3a", null ], [ "maneuverWindow", "structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.html#a05f53c65c42f0b02c07b80979dd2a440", null ], diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO-members.html b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO-members.html index 6f70603b..7b634e91 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO-members.html +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO-members.html @@ -90,7 +90,7 @@

This is the complete list of members for IO::SDK::API::DTO::ScenarioDTO, including all inherited members.

- + diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html index fef170e8..776cdf83 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html @@ -94,8 +94,8 @@
CelestialBodiesIO::SDK::API::DTO::ScenarioDTO
NameIO::SDK::API::DTO::ScenarioDTO
NameIO::SDK::API::DTO::ScenarioDTO
SitesIO::SDK::API::DTO::ScenarioDTO
SpacecraftIO::SDK::API::DTO::ScenarioDTO
WindowIO::SDK::API::DTO::ScenarioDTO
- - + + @@ -120,14 +120,14 @@

-

◆ Name

+ +

◆ Name

Public Attributes

char * Name {}
 
const char * Name {}
 
WindowDTO Window {}
 
SpacecraftDTO Spacecraft
- +
char* IO::SDK::API::DTO::ScenarioDTO::Name {}const char* IO::SDK::API::DTO::ScenarioDTO::Name {}
diff --git a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.js b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.js index fb67d332..8bcbf074 100644 --- a/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.js +++ b/Docs/html/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.js @@ -1,7 +1,7 @@ var structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO = [ [ "CelestialBodies", "structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html#a18b4ba7f3d152754f19ec3100381b8a0", null ], - [ "Name", "structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html#a46fecef09b2136f0d48b606cd0026430", null ], + [ "Name", "structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html#a19b9d3b85ddcc93df6029ea267ab1a85", null ], [ "Sites", "structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html#a232567cfa43075df51e869cd26d659cb", null ], [ "Spacecraft", "structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html#a1988e059e9da8f952ebd1e4602572f9c", null ], [ "Window", "structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.html#a36715d36708f0c714a8f6cdcfc232ad6", null ] diff --git a/Docs/latex/ApogeeHeightChangingManeuver_8cpp.tex b/Docs/latex/ApogeeHeightChangingManeuver_8cpp.tex index 9e1b74d8..6ada44ab 100644 --- a/Docs/latex/ApogeeHeightChangingManeuver_8cpp.tex +++ b/Docs/latex/ApogeeHeightChangingManeuver_8cpp.tex @@ -2,6 +2,7 @@ \label{ApogeeHeightChangingManeuver_8cpp}\index{IO.SDK/Maneuvers/ApogeeHeightChangingManeuver.cpp@{IO.SDK/Maneuvers/ApogeeHeightChangingManeuver.cpp}} {\ttfamily \#include $<$Apogee\+Height\+Changing\+Maneuver.\+h$>$}\newline {\ttfamily \#include $<$cmath$>$}\newline +{\ttfamily \#include $<$utility$>$}\newline {\ttfamily \#include $<$Parameters.\+h$>$}\newline diff --git a/Docs/latex/CombinedManeuver_8cpp.tex b/Docs/latex/CombinedManeuver_8cpp.tex index 9e977478..7bcc6f51 100644 --- a/Docs/latex/CombinedManeuver_8cpp.tex +++ b/Docs/latex/CombinedManeuver_8cpp.tex @@ -4,6 +4,7 @@ {\ttfamily \#include $<$Conic\+Orbital\+Elements.\+h$>$}\newline {\ttfamily \#include $<$Vector3\+D.\+h$>$}\newline {\ttfamily \#include $<$Parameters.\+h$>$}\newline +{\ttfamily \#include $<$utility$>$}\newline \doxysubsection{Detailed Description} diff --git a/Docs/latex/CombinedManeuver_8h_source.tex b/Docs/latex/CombinedManeuver_8h_source.tex index e36ac2a9..bdaa52c3 100644 --- a/Docs/latex/CombinedManeuver_8h_source.tex +++ b/Docs/latex/CombinedManeuver_8h_source.tex @@ -25,28 +25,27 @@ \DoxyCodeLine{30 \textcolor{keyword}{class }\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver}{CombinedManeuver}} final : \textcolor{keyword}{public} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1ManeuverBase}{IO::SDK::Maneuvers::ManeuverBase}}} \DoxyCodeLine{31 \{} \DoxyCodeLine{32 \textcolor{keyword}{private}:} -\DoxyCodeLine{33 \textcolor{keywordtype}{double} m\_relativeInclination\{\};} -\DoxyCodeLine{34 \textcolor{keywordtype}{double} m\_inclination;} -\DoxyCodeLine{35 \textcolor{keywordtype}{double} m\_peregeeRadius;} -\DoxyCodeLine{36 } -\DoxyCodeLine{37 [[nodiscard]] \mbox{\hyperlink{classIO_1_1SDK_1_1Math_1_1Vector3D}{IO::SDK::Math::Vector3D}} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1ManeuverBase_afa17b51d0c2bb7bd8f5abd2645664be8}{GetDeltaV}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector}{IO::SDK::OrbitalParameters::StateVector}}\& sv) \textcolor{keyword}{const};} -\DoxyCodeLine{38 } -\DoxyCodeLine{39 \textcolor{keyword}{protected}:} -\DoxyCodeLine{45 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver_a40963ff9fa4aff926dcbbe5e3b96e946}{Compute}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&maneuverPoint) \textcolor{keyword}{override};} -\DoxyCodeLine{46 } -\DoxyCodeLine{53 \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1StateOrientation}{IO::SDK::OrbitalParameters::StateOrientation}} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver_aa1430b3b1b33863ce6c7082dc8cb294f}{ComputeOrientation}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&maneuverPoint) \textcolor{keyword}{override};} -\DoxyCodeLine{54 } -\DoxyCodeLine{55 \textcolor{keyword}{public}:} -\DoxyCodeLine{60 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver_a0a13db037df238426af5e5420ab4e9bc}{CombinedManeuver}}(std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keywordtype}{double} inclination, \textcolor{keywordtype}{double} perigeeRadius);} -\DoxyCodeLine{61 } -\DoxyCodeLine{62 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver_a0a13db037df238426af5e5420ab4e9bc}{CombinedManeuver}}(std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keywordtype}{double} inclination, \textcolor{keywordtype}{double} perigeeRadius, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch);} -\DoxyCodeLine{63 } -\DoxyCodeLine{71 \textcolor{keywordtype}{bool} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver_a8e0b5838b45f0ab7abb381214eba5159}{CanExecute}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&orbitalParams) \textcolor{keyword}{override};} -\DoxyCodeLine{72 } -\DoxyCodeLine{73 \textcolor{keyword}{using }\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1ManeuverBase_afa17b51d0c2bb7bd8f5abd2645664be8}{IO::SDK::Maneuvers::ManeuverBase::GetDeltaV}};} -\DoxyCodeLine{74 \};} -\DoxyCodeLine{75 \}} -\DoxyCodeLine{76 } -\DoxyCodeLine{77 \textcolor{preprocessor}{\#endif}} +\DoxyCodeLine{33 \textcolor{keywordtype}{double} m\_inclination;} +\DoxyCodeLine{34 \textcolor{keywordtype}{double} m\_peregeeRadius;} +\DoxyCodeLine{35 } +\DoxyCodeLine{36 [[nodiscard]] \mbox{\hyperlink{classIO_1_1SDK_1_1Math_1_1Vector3D}{IO::SDK::Math::Vector3D}} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1ManeuverBase_afa17b51d0c2bb7bd8f5abd2645664be8}{GetDeltaV}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector}{IO::SDK::OrbitalParameters::StateVector}}\& sv) \textcolor{keyword}{const};} +\DoxyCodeLine{37 } +\DoxyCodeLine{38 \textcolor{keyword}{protected}:} +\DoxyCodeLine{44 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver_a40963ff9fa4aff926dcbbe5e3b96e946}{Compute}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&maneuverPoint) \textcolor{keyword}{override};} +\DoxyCodeLine{45 } +\DoxyCodeLine{52 \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1StateOrientation}{IO::SDK::OrbitalParameters::StateOrientation}} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver_aa1430b3b1b33863ce6c7082dc8cb294f}{ComputeOrientation}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&maneuverPoint) \textcolor{keyword}{override};} +\DoxyCodeLine{53 } +\DoxyCodeLine{54 \textcolor{keyword}{public}:} +\DoxyCodeLine{59 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver_a0a13db037df238426af5e5420ab4e9bc}{CombinedManeuver}}(std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keywordtype}{double} inclination, \textcolor{keywordtype}{double} perigeeRadius);} +\DoxyCodeLine{60 } +\DoxyCodeLine{61 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver_a0a13db037df238426af5e5420ab4e9bc}{CombinedManeuver}}(std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keywordtype}{double} inclination, \textcolor{keywordtype}{double} perigeeRadius, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch);} +\DoxyCodeLine{62 } +\DoxyCodeLine{70 \textcolor{keywordtype}{bool} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver_a8e0b5838b45f0ab7abb381214eba5159}{CanExecute}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&orbitalParams) \textcolor{keyword}{override};} +\DoxyCodeLine{71 } +\DoxyCodeLine{72 \textcolor{keyword}{using }\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1ManeuverBase_afa17b51d0c2bb7bd8f5abd2645664be8}{IO::SDK::Maneuvers::ManeuverBase::GetDeltaV}};} +\DoxyCodeLine{73 \};} +\DoxyCodeLine{74 \}} +\DoxyCodeLine{75 } +\DoxyCodeLine{76 \textcolor{preprocessor}{\#endif}} \end{DoxyCode} diff --git a/Docs/latex/Coordinate_8cpp.tex b/Docs/latex/Coordinate_8cpp.tex index 2a10cb43..ad1f8e18 100644 --- a/Docs/latex/Coordinate_8cpp.tex +++ b/Docs/latex/Coordinate_8cpp.tex @@ -1,6 +1,7 @@ \hypertarget{Coordinate_8cpp}{}\doxysection{IO.\+SDK/\+Coordinate.cpp File Reference} \label{Coordinate_8cpp}\index{IO.SDK/Coordinate.cpp@{IO.SDK/Coordinate.cpp}} {\ttfamily \#include $<$Coordinate.\+h$>$}\newline +{\ttfamily \#include $<$utility$>$}\newline {\ttfamily \#include \char`\"{}SDKException.\+h\char`\"{}}\newline diff --git a/Docs/latex/Coordinate_8h_source.tex b/Docs/latex/Coordinate_8h_source.tex index 2646b4b1..18e1a830 100644 --- a/Docs/latex/Coordinate_8h_source.tex +++ b/Docs/latex/Coordinate_8h_source.tex @@ -29,7 +29,7 @@ \DoxyCodeLine{34 } \DoxyCodeLine{35 \textcolor{keyword}{public}:} \DoxyCodeLine{36 } -\DoxyCodeLine{42 \textcolor{keyword}{explicit} \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_a14bc2970fed38a4ef4048cac18b7e716}{Coordinate}}(\textcolor{keyword}{const} std::string \&name);} +\DoxyCodeLine{42 \textcolor{keyword}{explicit} \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_ae1108a85782007065e647a88cad77365}{Coordinate}}(std::string name);} \DoxyCodeLine{43 \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_a1d592a91467a7d574105e8e29e8b5172}{\string~Coordinate}}() = \textcolor{keywordflow}{default};} \DoxyCodeLine{44 } \DoxyCodeLine{45 \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}} \&\mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_a48d76683e3f820e61293b3b300dd59ac}{operator=}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}} \&other)} @@ -55,7 +55,7 @@ \DoxyCodeLine{70 \textcolor{keyword}{static} \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}}\& \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_a267457ea043331d46b37a853603ac008}{RightAscension}}();} \DoxyCodeLine{71 \textcolor{keyword}{static} \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}}\& \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_af81aa1a4011d77113f4a1bc713800e50}{Declination}}();} \DoxyCodeLine{72 \textcolor{keyword}{static} \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}}\& \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_ab37d853fcae271174696a10c7fb95638}{Colatitude}}();} -\DoxyCodeLine{73 \textcolor{keyword}{static} \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}} \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_a76dca689301cabd728d6dd2b35e6f142}{ToCoordinateType}}(\textcolor{keyword}{const} std::string \&coordinateType) ;} +\DoxyCodeLine{73 \textcolor{keyword}{static} \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}}\& \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_a47227e958e970f8f289482c1fad15bba}{ToCoordinateType}}(\textcolor{keyword}{const} std::string \&coordinateType) ;} \DoxyCodeLine{74 \};} \DoxyCodeLine{75 } \DoxyCodeLine{76 \} \textcolor{comment}{// namespace IO::SDK}} diff --git a/Docs/latex/EngineDTO_8h_source.tex b/Docs/latex/EngineDTO_8h_source.tex index 571a6b4d..b2f9b51e 100644 --- a/Docs/latex/EngineDTO_8h_source.tex +++ b/Docs/latex/EngineDTO_8h_source.tex @@ -9,11 +9,11 @@ \DoxyCodeLine{5 \textcolor{keyword}{struct }\mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO}{EngineDTO}}} \DoxyCodeLine{6 \{} \DoxyCodeLine{7 \textcolor{keywordtype}{int} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_ae946e724e129f39d66841a6c60fb357f}{id}};} -\DoxyCodeLine{8 \textcolor{keywordtype}{char} * \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a37aaff67723471afe0b424b1c5f45b62}{serialNumber}};} -\DoxyCodeLine{9 \textcolor{keywordtype}{char} * \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a57fb452f92b221d0628df58fcec099dd}{fuelTankSerialNumber}};} -\DoxyCodeLine{10 \textcolor{keywordtype}{char} * \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a8eba4c4ea41e59883a38b5b31fc0c1cd}{name}};} +\DoxyCodeLine{8 \textcolor{keyword}{const} \textcolor{keywordtype}{char} * \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_aaaef37ff022681b8c013aabc22cf6bd3}{serialNumber}};} +\DoxyCodeLine{9 \textcolor{keyword}{const} \textcolor{keywordtype}{char} * \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_ae1586be547c6c629ef9fffa48ce3eb3e}{fuelTankSerialNumber}};} +\DoxyCodeLine{10 \textcolor{keyword}{const} \textcolor{keywordtype}{char} * \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_afba82457c3dba1f96881de6c7f96c6fc}{name}};} \DoxyCodeLine{11 \textcolor{keywordtype}{double} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a0ff30313e1775ad5bfcf6c290597bb83}{isp}};} -\DoxyCodeLine{12 \textcolor{keywordtype}{double} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a9a295704e9d53487bbbb3d11fc5e99e8}{fuelflow}};} +\DoxyCodeLine{12 \textcolor{keywordtype}{double} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_acb4c6108c1622e33f4b016ac6e933fe6}{fuelFlow}};} \DoxyCodeLine{13 \};} \DoxyCodeLine{14 } \DoxyCodeLine{15 \}} diff --git a/Docs/latex/FrameFile_8cpp.tex b/Docs/latex/FrameFile_8cpp.tex index 9f0aec36..642845a1 100644 --- a/Docs/latex/FrameFile_8cpp.tex +++ b/Docs/latex/FrameFile_8cpp.tex @@ -2,6 +2,7 @@ \label{FrameFile_8cpp}\index{IO.SDK/Frames/FrameFile.cpp@{IO.SDK/Frames/FrameFile.cpp}} {\ttfamily \#include $<$Frame\+File.\+h$>$}\newline {\ttfamily \#include $<$filesystem$>$}\newline +{\ttfamily \#include $<$utility$>$}\newline {\ttfamily \#include $<$Spice\+Usr.\+h$>$}\newline diff --git a/Docs/latex/FrameFile_8h_source.tex b/Docs/latex/FrameFile_8h_source.tex index af23cc90..a71005fb 100644 --- a/Docs/latex/FrameFile_8h_source.tex +++ b/Docs/latex/FrameFile_8h_source.tex @@ -17,7 +17,7 @@ \DoxyCodeLine{26 \textcolor{keyword}{const} std::string \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1FrameFile_abb7ceb3463eba84ab4513df3c0821055}{m\_filePath}}\{\};} \DoxyCodeLine{27 \textcolor{keywordtype}{bool} \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1FrameFile_aee3f358a8ff43053e026d84c5c999181}{m\_fileExists}}\{ \textcolor{keyword}{false} \};} \DoxyCodeLine{28 \textcolor{keywordtype}{bool} \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1FrameFile_ad375f342b427190d63e99ca903430497}{m\_isLoaded}}\{ \textcolor{keyword}{false} \};} -\DoxyCodeLine{29 \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1FrameFile_a7671ea08db5c6c165d75ec5760c0bd23}{FrameFile}}(\textcolor{keyword}{const} std::string\& filePath, \textcolor{keyword}{const} std::string\& name);} +\DoxyCodeLine{29 \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1FrameFile_aa66f02e3afdcd901dafed6661c8a1b28}{FrameFile}}(\textcolor{keyword}{const} std::string\& filePath, std::string name);} \DoxyCodeLine{30 \textcolor{keyword}{const} std::string \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1FrameFile_a9b0e652fc7622e68ff507dd69cc7eb47}{m\_name}}\{\};} \DoxyCodeLine{31 } \DoxyCodeLine{32 \textcolor{keyword}{public}:} diff --git a/Docs/latex/FuelTankDTO_8h_source.tex b/Docs/latex/FuelTankDTO_8h_source.tex index 485c9e18..9e7eeca9 100644 --- a/Docs/latex/FuelTankDTO_8h_source.tex +++ b/Docs/latex/FuelTankDTO_8h_source.tex @@ -9,7 +9,7 @@ \DoxyCodeLine{5 \textcolor{keyword}{struct }\mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO}{FuelTankDTO}}} \DoxyCodeLine{6 \{} \DoxyCodeLine{7 \textcolor{keywordtype}{int} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_ad511fe1e6898cc0280b0069f1f44207e}{id}};} -\DoxyCodeLine{8 \textcolor{keywordtype}{char} * \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_ad8aa5e4becba2f0767fa310849b8f1a1}{serialNumber}};} +\DoxyCodeLine{8 \textcolor{keyword}{const} \textcolor{keywordtype}{char} * \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_a52f3d0b45205f9b3e84f0bce316abe91}{serialNumber}};} \DoxyCodeLine{9 } \DoxyCodeLine{10 \textcolor{keywordtype}{double} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_aa8d92790c4185a373b2c013a2bb816ed}{capacity}};} \DoxyCodeLine{11 \textcolor{keywordtype}{double} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_a2e18763910cc002dfaccd86b1f23ef2e}{quantity}};} diff --git a/Docs/latex/GeometryFinder_8cpp.tex b/Docs/latex/GeometryFinder_8cpp.tex index 324ed53d..5594f13b 100644 --- a/Docs/latex/GeometryFinder_8cpp.tex +++ b/Docs/latex/GeometryFinder_8cpp.tex @@ -3,6 +3,4 @@ {\ttfamily \#include $<$Geometry\+Finder.\+h$>$}\newline {\ttfamily \#include $<$Spice\+Usr.\+h$>$}\newline {\ttfamily \#include $<$Builder.\+h$>$}\newline -{\ttfamily \#include \char`\"{}Celestial\+Body.\+h\char`\"{}}\newline {\ttfamily \#include \char`\"{}Illumination\+Angle.\+h\char`\"{}}\newline -{\ttfamily \#include $<$Helpers/\+Type.\+cpp$>$}\newline diff --git a/Docs/latex/Launch_8h_source.tex b/Docs/latex/Launch_8h_source.tex index 37d0ab9a..bd52076a 100644 --- a/Docs/latex/Launch_8h_source.tex +++ b/Docs/latex/Launch_8h_source.tex @@ -37,33 +37,32 @@ \DoxyCodeLine{42 \textcolor{keywordtype}{double} m\_inertialDescendingAzimuthLaunch\{std::numeric\_limits::quiet\_NaN()\};} \DoxyCodeLine{43 \textcolor{keywordtype}{double} m\_nonInertialDescendingAzimuthLaunch\{std::numeric\_limits::quiet\_NaN()\};} \DoxyCodeLine{44 \textcolor{keywordtype}{double} m\_nonInertialInsertionVelocity\{std::numeric\_limits::quiet\_NaN()\};} -\DoxyCodeLine{45 \textcolor{keywordtype}{double} m\_inertialInsertionVelocity\{std::numeric\_limits::quiet\_NaN()\};} -\DoxyCodeLine{46 } -\DoxyCodeLine{47 \textcolor{keyword}{const} \textcolor{keywordtype}{double} m\_deltaL\{std::numeric\_limits::quiet\_NaN()\};} -\DoxyCodeLine{48 \textcolor{keyword}{const} \textcolor{keywordtype}{double} m\_inclination\{std::numeric\_limits::quiet\_NaN()\};} -\DoxyCodeLine{49 } -\DoxyCodeLine{50 std::vector FindLaunchWindows(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1Window}{IO::SDK::Time::Window}} \&windowToSearch);} -\DoxyCodeLine{51 } -\DoxyCodeLine{52 \textcolor{keyword}{public}:} -\DoxyCodeLine{62 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a44abe43d2e13f901b07c20b238d71245}{Launch}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Sites_1_1LaunchSite}{IO::SDK::Sites::LaunchSite}}\& launchSite, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Sites_1_1Site}{IO::SDK::Sites::Site}}\& recoverySite, \textcolor{keywordtype}{bool} launchByDay, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&targetOrbit);} -\DoxyCodeLine{63 } -\DoxyCodeLine{69 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a2b6de32c8b88fc9b9d008a8cb326b06c}{GetNonInertialAscendingAzimuthLaunch}}();} -\DoxyCodeLine{70 } -\DoxyCodeLine{76 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_afb342ed1b11689e56fc87b416bdaab19}{GetNonInertialDescendingAzimuthLaunch}}();} -\DoxyCodeLine{77 } -\DoxyCodeLine{83 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a863826f45930d2f02b4a1f982f254de6}{GetInertialAscendingAzimuthLaunch}}();} -\DoxyCodeLine{84 } -\DoxyCodeLine{90 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a5eebdf15afcf84c0ca0a627c7900fabd}{GetInertialDescendingAzimuthLaunch}}();} -\DoxyCodeLine{91 } -\DoxyCodeLine{97 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a3a5a1efda97ebe4f84149dc9db4a1e09}{GetNonInertialInsertionVelocity}}();} -\DoxyCodeLine{98 } -\DoxyCodeLine{104 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_ac3ea597eb088b047a8c3a847d689180a}{GetInertialInsertionVelocity}}();} -\DoxyCodeLine{105 } -\DoxyCodeLine{112 std::vector \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a31298d41044193869b6ba40fc898617c}{GetLaunchWindows}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1Window}{IO::SDK::Time::Window}} \&searchWindow);} -\DoxyCodeLine{113 \};} -\DoxyCodeLine{114 } -\DoxyCodeLine{115 \} \textcolor{comment}{// namespace IO::SDK::Maneuvers}} -\DoxyCodeLine{116 } -\DoxyCodeLine{117 \textcolor{preprocessor}{\#endif }\textcolor{comment}{// LAUNCH\_MANEUVER\_H}} +\DoxyCodeLine{45 } +\DoxyCodeLine{46 \textcolor{keyword}{const} \textcolor{keywordtype}{double} m\_deltaL\{std::numeric\_limits::quiet\_NaN()\};} +\DoxyCodeLine{47 \textcolor{keyword}{const} \textcolor{keywordtype}{double} m\_inclination\{std::numeric\_limits::quiet\_NaN()\};} +\DoxyCodeLine{48 } +\DoxyCodeLine{49 std::vector FindLaunchWindows(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1Window}{IO::SDK::Time::Window}} \&windowToSearch);} +\DoxyCodeLine{50 } +\DoxyCodeLine{51 \textcolor{keyword}{public}:} +\DoxyCodeLine{61 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a44abe43d2e13f901b07c20b238d71245}{Launch}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Sites_1_1LaunchSite}{IO::SDK::Sites::LaunchSite}}\& launchSite, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Sites_1_1Site}{IO::SDK::Sites::Site}}\& recoverySite, \textcolor{keywordtype}{bool} launchByDay, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&targetOrbit);} +\DoxyCodeLine{62 } +\DoxyCodeLine{68 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a2b6de32c8b88fc9b9d008a8cb326b06c}{GetNonInertialAscendingAzimuthLaunch}}();} +\DoxyCodeLine{69 } +\DoxyCodeLine{75 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_afb342ed1b11689e56fc87b416bdaab19}{GetNonInertialDescendingAzimuthLaunch}}();} +\DoxyCodeLine{76 } +\DoxyCodeLine{82 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a863826f45930d2f02b4a1f982f254de6}{GetInertialAscendingAzimuthLaunch}}();} +\DoxyCodeLine{83 } +\DoxyCodeLine{89 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a5eebdf15afcf84c0ca0a627c7900fabd}{GetInertialDescendingAzimuthLaunch}}();} +\DoxyCodeLine{90 } +\DoxyCodeLine{96 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a3a5a1efda97ebe4f84149dc9db4a1e09}{GetNonInertialInsertionVelocity}}();} +\DoxyCodeLine{97 } +\DoxyCodeLine{103 \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_ac3ea597eb088b047a8c3a847d689180a}{GetInertialInsertionVelocity}}();} +\DoxyCodeLine{104 } +\DoxyCodeLine{111 std::vector \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Launch_a31298d41044193869b6ba40fc898617c}{GetLaunchWindows}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1Window}{IO::SDK::Time::Window}} \&searchWindow);} +\DoxyCodeLine{112 \};} +\DoxyCodeLine{113 } +\DoxyCodeLine{114 \} \textcolor{comment}{// namespace IO::SDK::Maneuvers}} +\DoxyCodeLine{115 } +\DoxyCodeLine{116 \textcolor{preprocessor}{\#endif }\textcolor{comment}{// LAUNCH\_MANEUVER\_H}} \end{DoxyCode} diff --git a/Docs/latex/NadirAttitude_8h_source.tex b/Docs/latex/NadirAttitude_8h_source.tex index d4d492f8..37a79a59 100644 --- a/Docs/latex/NadirAttitude_8h_source.tex +++ b/Docs/latex/NadirAttitude_8h_source.tex @@ -29,9 +29,9 @@ \DoxyCodeLine{45 \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1StateOrientation}{IO::SDK::OrbitalParameters::StateOrientation}} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_ad6c8b02e0d98d55a3f047a67638261cd}{ComputeOrientation}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&maneuverPoint) \textcolor{keyword}{override};} \DoxyCodeLine{46 } \DoxyCodeLine{47 \textcolor{keyword}{public}:} -\DoxyCodeLine{54 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a1c42b8b24041b935c7c39ff8713659da}{NadirAttitude}}(\textcolor{keyword}{const} std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} +\DoxyCodeLine{54 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a19100017abcc10cbc88c768ad3d83c8c}{NadirAttitude}}(\textcolor{keyword}{const} std::vector\& engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} \DoxyCodeLine{55 } -\DoxyCodeLine{63 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a1c42b8b24041b935c7c39ff8713659da}{NadirAttitude}}(\textcolor{keyword}{const} std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} +\DoxyCodeLine{63 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a19100017abcc10cbc88c768ad3d83c8c}{NadirAttitude}}(\textcolor{keyword}{const} std::vector\& engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} \DoxyCodeLine{64 } \DoxyCodeLine{72 \textcolor{keywordtype}{bool} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a9f7b6b754fcf56017f44c1499a3decb1}{CanExecute}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&orbitalParams) \textcolor{keyword}{override};} \DoxyCodeLine{73 \};} diff --git a/Docs/latex/OrbitalParameters_8cpp.tex b/Docs/latex/OrbitalParameters_8cpp.tex index 32b1c079..1b026de5 100644 --- a/Docs/latex/OrbitalParameters_8cpp.tex +++ b/Docs/latex/OrbitalParameters_8cpp.tex @@ -4,6 +4,7 @@ {\ttfamily \#include $<$State\+Vector.\+h$>$}\newline {\ttfamily \#include $<$Inertial\+Frames.\+h$>$}\newline {\ttfamily \#include $<$Parameters.\+h$>$}\newline +{\ttfamily \#include $<$utility$>$}\newline \doxysubsection{Detailed Description} diff --git a/Docs/latex/OrbitalParameters_8h_source.tex b/Docs/latex/OrbitalParameters_8h_source.tex index 675a5ef1..fdac18c7 100644 --- a/Docs/latex/OrbitalParameters_8h_source.tex +++ b/Docs/latex/OrbitalParameters_8h_source.tex @@ -30,7 +30,7 @@ \DoxyCodeLine{39 \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1Frames}{IO::SDK::Frames::Frames}} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_ac0945ce17c2c770916aaf694f5557437}{m\_frame}};} \DoxyCodeLine{40 } \DoxyCodeLine{41 \textcolor{keyword}{public}:} -\DoxyCodeLine{49 \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_aa2ad5e93197a2465c3cf50b8065f6d61}{OrbitalParameters}}(\textcolor{keyword}{const} std::shared\_ptr \¢erOfMotion, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&epoch, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1Frames}{IO::SDK::Frames::Frames}} \&frame);} +\DoxyCodeLine{49 \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_a2e151aad0e34a4bc0918f93ec536ea58}{OrbitalParameters}}(\textcolor{keyword}{const} std::shared\_ptr \¢erOfMotion, \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} epoch, \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1Frames}{IO::SDK::Frames::Frames}} frame);} \DoxyCodeLine{50 } \DoxyCodeLine{51 \textcolor{keyword}{virtual} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_a4c24cb357f03afe566885b46b86797c0}{\string~OrbitalParameters}}() = \textcolor{keywordflow}{default};} \DoxyCodeLine{52 } diff --git a/Docs/latex/OrbitalPlaneChangingManeuverDTO_8h_source.tex b/Docs/latex/OrbitalPlaneChangingManeuverDTO_8h_source.tex index b479cd54..d38adf09 100644 --- a/Docs/latex/OrbitalPlaneChangingManeuverDTO_8h_source.tex +++ b/Docs/latex/OrbitalPlaneChangingManeuverDTO_8h_source.tex @@ -17,7 +17,7 @@ \DoxyCodeLine{13 \textcolor{keyword}{struct }\mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO}{OrbitalPlaneChangingManeuverDTO}}} \DoxyCodeLine{14 \{} \DoxyCodeLine{15 \textcolor{keywordtype}{int} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_a8c9d63e641f8ec865cc7c8e7369b0f3a}{maneuverOrder}}\{-\/1\};} -\DoxyCodeLine{16 \textcolor{keywordtype}{char}* \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ac92b335a51002a99f037eaf11fe0cf1c}{engines}}[5]\{\};} +\DoxyCodeLine{16 \textcolor{keyword}{const} \textcolor{keywordtype}{char}* \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ac68a3c6f143c4e2468ddeb1d6d091e99}{engines}}[5]\{\};} \DoxyCodeLine{17 \textcolor{keywordtype}{double} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ae949350a0a86deccbc35378e75a73e80}{attitudeHoldDuration}}\{0.0\};} \DoxyCodeLine{18 \textcolor{keywordtype}{double} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ae3b703ef40ec48ba3b1091e09eaa688f}{minimumEpoch}}\{0.0\};} \DoxyCodeLine{19 } diff --git a/Docs/latex/PerigeeHeightChangingManeuver_8cpp.tex b/Docs/latex/PerigeeHeightChangingManeuver_8cpp.tex index e032884d..1a6d48ce 100644 --- a/Docs/latex/PerigeeHeightChangingManeuver_8cpp.tex +++ b/Docs/latex/PerigeeHeightChangingManeuver_8cpp.tex @@ -3,6 +3,7 @@ {\ttfamily \#include $<$Perigee\+Height\+Changing\+Maneuver.\+h$>$}\newline {\ttfamily \#include $<$Constants.\+h$>$}\newline {\ttfamily \#include $<$Parameters.\+h$>$}\newline +{\ttfamily \#include $<$utility$>$}\newline \doxysubsection{Detailed Description} diff --git a/Docs/latex/ProgradeAttitude_8h_source.tex b/Docs/latex/ProgradeAttitude_8h_source.tex index b0889762..c346c1bb 100644 --- a/Docs/latex/ProgradeAttitude_8h_source.tex +++ b/Docs/latex/ProgradeAttitude_8h_source.tex @@ -28,9 +28,9 @@ \DoxyCodeLine{44 \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1StateOrientation}{IO::SDK::OrbitalParameters::StateOrientation}} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a794ab49935a4feced62692674ea8109d}{ComputeOrientation}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&maneuverPoint) \textcolor{keyword}{override};} \DoxyCodeLine{45 } \DoxyCodeLine{46 \textcolor{keyword}{public}:} -\DoxyCodeLine{53 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a4befd3aa292dd8185e87c1f7b62f22c0}{ProgradeAttitude}}(\textcolor{keyword}{const} std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} +\DoxyCodeLine{53 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a73af1392368d15c48ee2f892eef72f34}{ProgradeAttitude}}(\textcolor{keyword}{const} std::vector\& engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} \DoxyCodeLine{54 } -\DoxyCodeLine{62 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a4befd3aa292dd8185e87c1f7b62f22c0}{ProgradeAttitude}}(\textcolor{keyword}{const} std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} +\DoxyCodeLine{62 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a73af1392368d15c48ee2f892eef72f34}{ProgradeAttitude}}(\textcolor{keyword}{const} std::vector\& engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} \DoxyCodeLine{63 } \DoxyCodeLine{71 \textcolor{keywordtype}{bool} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_acc05df379c165ce5052799888f9e3719}{CanExecute}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&orbitalParams) \textcolor{keyword}{override};} \DoxyCodeLine{72 \};} diff --git a/Docs/latex/Propagator_8cpp.tex b/Docs/latex/Propagator_8cpp.tex index b31337a3..5b2d242f 100644 --- a/Docs/latex/Propagator_8cpp.tex +++ b/Docs/latex/Propagator_8cpp.tex @@ -2,7 +2,6 @@ \label{Propagator_8cpp}\index{IO.SDK/Propagators/Propagator.cpp@{IO.SDK/Propagators/Propagator.cpp}} {\ttfamily \#include $<$Propagator.\+h$>$}\newline {\ttfamily \#include $<$Propagator\+Exception.\+h$>$}\newline -{\ttfamily \#include $<$algorithm$>$}\newline {\ttfamily \#include $<$Maneuver\+Base.\+h$>$}\newline {\ttfamily \#include $<$State\+Orientation.\+h$>$}\newline diff --git a/Docs/latex/Proxy_8h_source.tex b/Docs/latex/Proxy_8h_source.tex index 84d896b4..bbffe01e 100644 --- a/Docs/latex/Proxy_8h_source.tex +++ b/Docs/latex/Proxy_8h_source.tex @@ -87,7 +87,7 @@ \DoxyCodeLine{216 \textcolor{preprocessor}{\#ifdef \_\_cplusplus}} \DoxyCodeLine{217 \}} \DoxyCodeLine{218 \textcolor{preprocessor}{\#endif}} -\DoxyCodeLine{219 \textcolor{preprocessor}{\#pragma endregion}} +\DoxyCodeLine{219 \textcolor{preprocessor}{\#pragma endregion Proxy}} \DoxyCodeLine{220 } \DoxyCodeLine{221 \textcolor{preprocessor}{\#ifndef PROXY\_H}} \DoxyCodeLine{222 \textcolor{preprocessor}{\#define PROXY\_H}} diff --git a/Docs/latex/RelationnalOperator_8cpp.tex b/Docs/latex/RelationnalOperator_8cpp.tex index 3d469bbb..13a8467f 100644 --- a/Docs/latex/RelationnalOperator_8cpp.tex +++ b/Docs/latex/RelationnalOperator_8cpp.tex @@ -2,5 +2,4 @@ \label{RelationnalOperator_8cpp}\index{IO.SDK/Constraints/RelationnalOperator.cpp@{IO.SDK/Constraints/RelationnalOperator.cpp}} {\ttfamily \#include \char`\"{}Relational\+Operator.\+h\char`\"{}}\newline {\ttfamily \#include $<$utility$>$}\newline -{\ttfamily \#include $<$cstring$>$}\newline {\ttfamily \#include $<$SDKException.\+h$>$}\newline diff --git a/Docs/latex/RetrogradeAttitude_8h_source.tex b/Docs/latex/RetrogradeAttitude_8h_source.tex index a1450dc6..8894442f 100644 --- a/Docs/latex/RetrogradeAttitude_8h_source.tex +++ b/Docs/latex/RetrogradeAttitude_8h_source.tex @@ -28,9 +28,9 @@ \DoxyCodeLine{44 \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1StateOrientation}{IO::SDK::OrbitalParameters::StateOrientation}} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a8f938d701ccc27bd757bd1017e3561c7}{ComputeOrientation}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&maneuverPoint) \textcolor{keyword}{override};} \DoxyCodeLine{45 } \DoxyCodeLine{46 \textcolor{keyword}{public}:} -\DoxyCodeLine{53 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a3867ab497cd0e694917d20e9d9a43334}{RetrogradeAttitude}}(\textcolor{keyword}{const} std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} +\DoxyCodeLine{53 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a1c0f94622fa6b2c3641afe8a51da367b}{RetrogradeAttitude}}(\textcolor{keyword}{const} std::vector\& engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} \DoxyCodeLine{54 } -\DoxyCodeLine{62 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a3867ab497cd0e694917d20e9d9a43334}{RetrogradeAttitude}}(\textcolor{keyword}{const} std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} +\DoxyCodeLine{62 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a1c0f94622fa6b2c3641afe8a51da367b}{RetrogradeAttitude}}(\textcolor{keyword}{const} std::vector\& engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration);} \DoxyCodeLine{63 } \DoxyCodeLine{71 \textcolor{keywordtype}{bool} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_ace8726c7e00edf44bb790be5050a7f24}{CanExecute}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&orbitalParams) \textcolor{keyword}{override};} \DoxyCodeLine{72 \};} diff --git a/Docs/latex/ScenarioDTO_8h_source.tex b/Docs/latex/ScenarioDTO_8h_source.tex index 56fc6358..061c2071 100644 --- a/Docs/latex/ScenarioDTO_8h_source.tex +++ b/Docs/latex/ScenarioDTO_8h_source.tex @@ -13,7 +13,7 @@ \DoxyCodeLine{9 \{} \DoxyCodeLine{10 \textcolor{keyword}{struct }\mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO}{ScenarioDTO}}} \DoxyCodeLine{11 \{} -\DoxyCodeLine{12 \textcolor{keywordtype}{char} *\mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a46fecef09b2136f0d48b606cd0026430}{Name}}\{\};} +\DoxyCodeLine{12 \textcolor{keyword}{const} \textcolor{keywordtype}{char} *\mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a19b9d3b85ddcc93df6029ea267ab1a85}{Name}}\{\};} \DoxyCodeLine{13 \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1WindowDTO}{WindowDTO}} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a36715d36708f0c714a8f6cdcfc232ad6}{Window}}\{\};} \DoxyCodeLine{14 \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1SpacecraftDTO}{SpacecraftDTO}} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a1988e059e9da8f952ebd1e4602572f9c}{Spacecraft}};} \DoxyCodeLine{15 \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1SiteDTO}{SiteDTO}} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a232567cfa43075df51e869cd26d659cb}{Sites}}[10];} diff --git a/Docs/latex/Scenario_8h_source.tex b/Docs/latex/Scenario_8h_source.tex index a9c89b4a..52bc815a 100644 --- a/Docs/latex/Scenario_8h_source.tex +++ b/Docs/latex/Scenario_8h_source.tex @@ -81,27 +81,11 @@ \DoxyCodeLine{113 \textcolor{keyword}{inline} \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{Propagators::Propagator}} \&\mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_aeee297b71c3a8eeabdf538e24ad7182a}{GetPropagator}}()} \DoxyCodeLine{114 \{ \textcolor{keywordflow}{return} *m\_propagator; \}} \DoxyCodeLine{115 } -\DoxyCodeLine{116 } -\DoxyCodeLine{117 } -\DoxyCodeLine{122 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a1edecc4b70536953805561cfcb6f263f}{AddDistanceConstraint}}(Constraints::Parameters::DistanceParameters *distanceParameters);} +\DoxyCodeLine{119 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a5023a3fec59ef54ca3d1f301d8313d19}{Execute}}();} +\DoxyCodeLine{120 \};} +\DoxyCodeLine{121 } +\DoxyCodeLine{122 \} \textcolor{comment}{// IO::SDK}} \DoxyCodeLine{123 } -\DoxyCodeLine{128 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_ad90005ecbd0ec3bf596c81e4758023d7}{AddOccultationConstraint}}(IO::SDK::Constraints::Parameters::OccultationParameters *occultationParameters);} -\DoxyCodeLine{129 } -\DoxyCodeLine{134 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_ac87ca28b5c56abea86b626a6067e9e03}{AddDayConstraint}}(IO::SDK::Constraints::Parameters::ByDayParameters *byDayParameters);} -\DoxyCodeLine{135 } -\DoxyCodeLine{140 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_aefd1fe0c77211b597e71599be8f8482a}{AddNightConstraint}}(IO::SDK::Constraints::Parameters::ByNightParameters *byNightParameters);} -\DoxyCodeLine{141 } -\DoxyCodeLine{146 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a38fb82b4679d789a253bcfa29ef627d4}{AddBodyVisibilityConstraint}}(IO::SDK::Constraints::Parameters::BodyVisibilityFromSiteParameters *bodyVisibilityParameters);} -\DoxyCodeLine{147 } -\DoxyCodeLine{152 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a0e3cd3bf3d3e6a238cf2c69ced4b922e}{AddInFieldOfViewConstraint}}(IO::SDK::Constraints::Parameters::InFieldOfViewParameters *inFieldOfViewParameters);} -\DoxyCodeLine{153 } -\DoxyCodeLine{158 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a48c2803d92a0487167a9490dc75c4aac}{AddLaunchConstraint}}(IO::SDK::Constraints::Parameters::LaunchParameters *launchParameters);} -\DoxyCodeLine{159 } -\DoxyCodeLine{163 \textcolor{keywordtype}{void} \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a5023a3fec59ef54ca3d1f301d8313d19}{Execute}}();} -\DoxyCodeLine{164 \};} -\DoxyCodeLine{165 } -\DoxyCodeLine{166 \} \textcolor{comment}{// IO::SDK}} -\DoxyCodeLine{167 } -\DoxyCodeLine{168 \textcolor{preprocessor}{\#endif }\textcolor{comment}{//IOSDK\_SCENARIO\_H}} +\DoxyCodeLine{124 \textcolor{preprocessor}{\#endif }\textcolor{comment}{//IOSDK\_SCENARIO\_H}} \end{DoxyCode} diff --git a/Docs/latex/Spacecraft_8h_source.tex b/Docs/latex/Spacecraft_8h_source.tex index 4e02cf50..430be748 100644 --- a/Docs/latex/Spacecraft_8h_source.tex +++ b/Docs/latex/Spacecraft_8h_source.tex @@ -147,8 +147,8 @@ \DoxyCodeLine{337 } \DoxyCodeLine{342 \textcolor{keyword}{const} std::unique\_ptr \&\mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_ab7108bea66420d9274c50e206cce5524}{GetFrame}}() \textcolor{keyword}{const};} \DoxyCodeLine{343 } -\DoxyCodeLine{344 \textcolor{keyword}{inline} \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_aebe8482d25128fdb0e64466e68c84609}{GetMaximumOperatingMass}}()} -\DoxyCodeLine{345 \{ \textcolor{keywordflow}{return} m\_maximumOperatingMass; \}} +\DoxyCodeLine{344 \textcolor{keyword}{inline} \textcolor{keywordtype}{double} \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_ab83dd50751732be26d21cff147fcd548}{GetMaximumOperatingMass}}()\textcolor{keyword}{ const}} +\DoxyCodeLine{345 \textcolor{keyword}{ }\{ \textcolor{keywordflow}{return} m\_maximumOperatingMass; \}} \DoxyCodeLine{346 \};} \DoxyCodeLine{347 \}} \DoxyCodeLine{348 } diff --git a/Docs/latex/TowardObjectAttitude_8h_source.tex b/Docs/latex/TowardObjectAttitude_8h_source.tex index 11f06b49..5060ea0f 100644 --- a/Docs/latex/TowardObjectAttitude_8h_source.tex +++ b/Docs/latex/TowardObjectAttitude_8h_source.tex @@ -28,9 +28,9 @@ \DoxyCodeLine{44 \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1StateOrientation}{IO::SDK::OrbitalParameters::StateOrientation}} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a2296926c7cc97c3d118181b802f3720c}{ComputeOrientation}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&maneuverPoint) \textcolor{keyword}{override};} \DoxyCodeLine{45 } \DoxyCodeLine{46 \textcolor{keyword}{public}:} -\DoxyCodeLine{54 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a4f54adecfccb8b73e08a0bf8aef7dccb}{TowardObjectAttitude}}(\textcolor{keyword}{const} std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO::SDK::Body::Body}} \&targetBody);} +\DoxyCodeLine{54 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a6a1d2837006c792f1416441e4311c3ce}{TowardObjectAttitude}}(\textcolor{keyword}{const} std::vector\& engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO::SDK::Body::Body}} \&targetBody);} \DoxyCodeLine{55 } -\DoxyCodeLine{64 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a4f54adecfccb8b73e08a0bf8aef7dccb}{TowardObjectAttitude}}(\textcolor{keyword}{const} std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO::SDK::Body::Body}} \&targetBody);} +\DoxyCodeLine{64 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a6a1d2837006c792f1416441e4311c3ce}{TowardObjectAttitude}}(\textcolor{keyword}{const} std::vector\& engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch,\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}}\& attitudeHoldDuration, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO::SDK::Body::Body}} \&targetBody);} \DoxyCodeLine{65 } \DoxyCodeLine{73 \textcolor{keywordtype}{bool} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a8d3620611d4b1983dfc2a15fbb9b1128}{CanExecute}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&orbitalParams) \textcolor{keyword}{override};} \DoxyCodeLine{74 \};} diff --git a/Docs/latex/ZenithAttitude_8h_source.tex b/Docs/latex/ZenithAttitude_8h_source.tex index f34b2c7f..e9530ad4 100644 --- a/Docs/latex/ZenithAttitude_8h_source.tex +++ b/Docs/latex/ZenithAttitude_8h_source.tex @@ -28,9 +28,9 @@ \DoxyCodeLine{44 \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1StateOrientation}{IO::SDK::OrbitalParameters::StateOrientation}} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_adb59be8151c3be823650ed5a0f1d16f4}{ComputeOrientation}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&maneuverPoint) \textcolor{keyword}{override};} \DoxyCodeLine{45 } \DoxyCodeLine{46 \textcolor{keyword}{public}:} -\DoxyCodeLine{53 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a3dfe74492c2bed032f37ac4d02e153be}{ZenithAttitude}}(\textcolor{keyword}{const} std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}} \&attitudeHoldDuration);} +\DoxyCodeLine{53 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a75359142c87e83ac94578e3b92242239}{ZenithAttitude}}(\textcolor{keyword}{const} std::vector\& engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}} \&attitudeHoldDuration);} \DoxyCodeLine{54 } -\DoxyCodeLine{62 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a3dfe74492c2bed032f37ac4d02e153be}{ZenithAttitude}}(\textcolor{keyword}{const} std::vector engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}} \&attitudeHoldDuration);} +\DoxyCodeLine{62 \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a75359142c87e83ac94578e3b92242239}{ZenithAttitude}}(\textcolor{keyword}{const} std::vector\& engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO::SDK::Propagators::Propagator}} \&propagator, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO::SDK::Time::TDB}} \&minimumEpoch, \textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO::SDK::Time::TimeSpan}} \&attitudeHoldDuration);} \DoxyCodeLine{63 } \DoxyCodeLine{71 \textcolor{keywordtype}{bool} \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a02199451b76c086541d3a99f5032ed84}{CanExecute}}(\textcolor{keyword}{const} \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO::SDK::OrbitalParameters::OrbitalParameters}} \&orbitalParams) \textcolor{keyword}{override};} \DoxyCodeLine{72 \};} diff --git a/Docs/latex/classIO_1_1SDK_1_1Body_1_1Body.pdf b/Docs/latex/classIO_1_1SDK_1_1Body_1_1Body.pdf index 80053ec2a47d0da1638832445c0fa8de351de2e2..39e9f099488f501b76b4b91bbf408a50bedeb3ac 100644 GIT binary patch delta 200 zcmca)a>-^a} E0D+M(iU0rr delta 200 zcmca)a>-9)ZO-+prT`f$_ES+2pT^a} E06pR`i~s-t diff --git a/Docs/latex/classIO_1_1SDK_1_1Body_1_1CelestialBody.pdf b/Docs/latex/classIO_1_1SDK_1_1Body_1_1CelestialBody.pdf index 139d518b0c498d589dd035ce64b2839c259eb9ee..82f9df4c07bb88717b8753a173897494577e8a55 100644 GIT binary patch delta 177 zcmeA%>M`1IRhZkzJjBq%%GAKh*l6+tVFMJtw8#!#%M?q~w6x?@U1O6(%gql&teCWn z%neOU4UCPn4UE(c4AeEb^nLSFToOxCHC(KW42+BoOkpZEyNG8qIvF_{8yZ`<8CsgS iSh^UP8XLMfTevtHI2yS)nHd`xJKNb1QZf0XgfsvT+boCx delta 177 zcmeA%>M`1IRhZk*GQ`l-%Ea8tz-;mZVFMJtw8#!#V?z^TW5YB9U87Vpi_H&2teCV6 zEe%ag%ni)64UE(c4AeEb^nLSFToOxCHC(KW42+BoOkpZEyNG8qI=Q+SJ6Re!8aunW ixwsjaIvTjRn46dzyP6xBnK&9anb_G7QZf0XgfsxkwJb;g diff --git a/Docs/latex/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.pdf b/Docs/latex/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.pdf index 541d6114161e1844cb20d9c18a2fbbebcff6d55b..1777cc7a2139b8d4c80ffc355e5851a6215fc821 100644 GIT binary patch delta 156 zcmexn^v!64y$H9Fd5EEjm8pT1vC(8N5d#!{tH=&s%M?q~w6x?@U1O6(%gtV*R!kg5 z=7uJw20-;a;!<$V=5^xPj7|mymWGDrhNiBjrWOWfW`-_~h6d&auI7dYt_BvyW=?iC Lgj7t9mXrnncXuX5 delta 156 zcmexn^v!64y$H9VWr(4vm5I5Pf!Sm)5d#!{tH=&sV?z^TW5YB9U87Vpi_Ko5R!kg* zmWHM#=0Np5;!<$V=5^xPj83lR#^&ZGCPt2qE=GoKmIj6Vf diff --git a/Docs/latex/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.tex b/Docs/latex/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.tex index b1374c92..e3d83681 100644 --- a/Docs/latex/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.tex +++ b/Docs/latex/classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft.tex @@ -76,7 +76,7 @@ \begin{DoxyCompactList}\small\item\em Get the Dry Operating Mass object. \end{DoxyCompactList}\item const std\+::unique\+\_\+ptr$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1SpacecraftFrameFile}{IO\+::\+SDK\+::\+Frames\+::\+Spacecraft\+Frame\+File}} $>$ \& \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_ab7108bea66420d9274c50e206cce5524}{Get\+Frame}} () const \item -double \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_aebe8482d25128fdb0e64466e68c84609}{Get\+Maximum\+Operating\+Mass}} () +double \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_ab83dd50751732be26d21cff147fcd548}{Get\+Maximum\+Operating\+Mass}} () const \end{DoxyCompactItemize} \doxysubsection*{Public Attributes} \begin{DoxyCompactItemize} @@ -445,11 +445,11 @@ Reimplemented from \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body_a166ce7048ed87d61f6f40b51e5d4f609}{IO\+::\+SDK\+::\+Body\+::\+Body}}. -\mbox{\Hypertarget{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_aebe8482d25128fdb0e64466e68c84609}\label{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_aebe8482d25128fdb0e64466e68c84609}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_ab83dd50751732be26d21cff147fcd548}\label{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_ab83dd50751732be26d21cff147fcd548}} \index{IO::SDK::Body::Spacecraft::Spacecraft@{IO::SDK::Body::Spacecraft::Spacecraft}!GetMaximumOperatingMass@{GetMaximumOperatingMass}} \index{GetMaximumOperatingMass@{GetMaximumOperatingMass}!IO::SDK::Body::Spacecraft::Spacecraft@{IO::SDK::Body::Spacecraft::Spacecraft}} \doxysubsubsection{\texorpdfstring{GetMaximumOperatingMass()}{GetMaximumOperatingMass()}} -{\footnotesize\ttfamily double IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Spacecraft\+::\+Get\+Maximum\+Operating\+Mass (\begin{DoxyParamCaption}{ }\end{DoxyParamCaption})\hspace{0.3cm}{\ttfamily [inline]}} +{\footnotesize\ttfamily double IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Spacecraft\+::\+Get\+Maximum\+Operating\+Mass (\begin{DoxyParamCaption}{ }\end{DoxyParamCaption}) const\hspace{0.3cm}{\ttfamily [inline]}} \mbox{\Hypertarget{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_ababce78d27520ce4fe4ee9a86ff5049b}\label{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Spacecraft_ababce78d27520ce4fe4ee9a86ff5049b}} \index{IO::SDK::Body::Spacecraft::Spacecraft@{IO::SDK::Body::Spacecraft::Spacecraft}!GetOrientation@{GetOrientation}} diff --git a/Docs/latex/classIO_1_1SDK_1_1Coordinate.tex b/Docs/latex/classIO_1_1SDK_1_1Coordinate.tex index 1f2f4e66..ac4c87e2 100644 --- a/Docs/latex/classIO_1_1SDK_1_1Coordinate.tex +++ b/Docs/latex/classIO_1_1SDK_1_1Coordinate.tex @@ -7,7 +7,7 @@ \doxysubsection*{Public Member Functions} \begin{DoxyCompactItemize} \item -\mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_a14bc2970fed38a4ef4048cac18b7e716}{Coordinate}} (const std\+::string \&name) +\mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_ae1108a85782007065e647a88cad77365}{Coordinate}} (std\+::string name) \begin{DoxyCompactList}\small\item\em Construct a new \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}} object. \end{DoxyCompactList}\item \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_a1d592a91467a7d574105e8e29e8b5172}{$\sim$\+Coordinate}} ()=default \item @@ -40,16 +40,16 @@ \item static \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}} \& \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_ab37d853fcae271174696a10c7fb95638}{Colatitude}} () \item -static \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}} \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_a76dca689301cabd728d6dd2b35e6f142}{To\+Coordinate\+Type}} (const std\+::string \&coordinate\+Type) +static \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{Coordinate}} \& \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate_a47227e958e970f8f289482c1fad15bba}{To\+Coordinate\+Type}} (const std\+::string \&coordinate\+Type) \end{DoxyCompactItemize} \doxysubsection{Constructor \& Destructor Documentation} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Coordinate_a14bc2970fed38a4ef4048cac18b7e716}\label{classIO_1_1SDK_1_1Coordinate_a14bc2970fed38a4ef4048cac18b7e716}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Coordinate_ae1108a85782007065e647a88cad77365}\label{classIO_1_1SDK_1_1Coordinate_ae1108a85782007065e647a88cad77365}} \index{IO::SDK::Coordinate@{IO::SDK::Coordinate}!Coordinate@{Coordinate}} \index{Coordinate@{Coordinate}!IO::SDK::Coordinate@{IO::SDK::Coordinate}} \doxysubsubsection{\texorpdfstring{Coordinate()}{Coordinate()}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Coordinate\+::\+Coordinate (\begin{DoxyParamCaption}\item[{const std\+::string \&}]{name }\end{DoxyParamCaption})\hspace{0.3cm}{\ttfamily [explicit]}} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Coordinate\+::\+Coordinate (\begin{DoxyParamCaption}\item[{std\+::string}]{name }\end{DoxyParamCaption})\hspace{0.3cm}{\ttfamily [explicit]}} @@ -136,11 +136,11 @@ \begin{DoxyReturn}{Returns} const char$\ast$ \end{DoxyReturn} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Coordinate_a76dca689301cabd728d6dd2b35e6f142}\label{classIO_1_1SDK_1_1Coordinate_a76dca689301cabd728d6dd2b35e6f142}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Coordinate_a47227e958e970f8f289482c1fad15bba}\label{classIO_1_1SDK_1_1Coordinate_a47227e958e970f8f289482c1fad15bba}} \index{IO::SDK::Coordinate@{IO::SDK::Coordinate}!ToCoordinateType@{ToCoordinateType}} \index{ToCoordinateType@{ToCoordinateType}!IO::SDK::Coordinate@{IO::SDK::Coordinate}} \doxysubsubsection{\texorpdfstring{ToCoordinateType()}{ToCoordinateType()}} -{\footnotesize\ttfamily \mbox{\hyperlink{classIO_1_1SDK_1_1Coordinate}{IO\+::\+SDK\+::\+Coordinate}} IO\+::\+SDK\+::\+Coordinate\+::\+To\+Coordinate\+Type (\begin{DoxyParamCaption}\item[{const std\+::string \&}]{coordinate\+Type }\end{DoxyParamCaption})\hspace{0.3cm}{\ttfamily [static]}} +{\footnotesize\ttfamily 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\mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) +\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a19100017abcc10cbc88c768ad3d83c8c}{Nadir\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) \begin{DoxyCompactList}\small\item\em Construct a new Nadir Attitude object. \end{DoxyCompactList}\item -\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_af72bad35d416092ca326ca93906757c7}{Nadir\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&minimum\+Epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) +\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_aff17952207dcb51f47cc93fedb0b20fb}{Nadir\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&minimum\+Epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) \begin{DoxyCompactList}\small\item\em Construct a new Nadir Attitude object. \end{DoxyCompactList}\item bool \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a9f7b6b754fcf56017f44c1499a3decb1}{Can\+Execute}} (const \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO\+::\+SDK\+::\+Orbital\+Parameters\+::\+Orbital\+Parameters}} \&orbital\+Params) override \begin{DoxyCompactList}\small\item\em Evaluate if maneuver can occurs. \end{DoxyCompactList}\end{DoxyCompactItemize} @@ -30,11 +30,11 @@ \doxysubsection{Constructor \& Destructor Documentation} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a1c42b8b24041b935c7c39ff8713659da}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a1c42b8b24041b935c7c39ff8713659da}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a19100017abcc10cbc88c768ad3d83c8c}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_a19100017abcc10cbc88c768ad3d83c8c}} \index{IO::SDK::Maneuvers::Attitudes::NadirAttitude@{IO::SDK::Maneuvers::Attitudes::NadirAttitude}!NadirAttitude@{NadirAttitude}} \index{NadirAttitude@{NadirAttitude}!IO::SDK::Maneuvers::Attitudes::NadirAttitude@{IO::SDK::Maneuvers::Attitudes::NadirAttitude}} \doxysubsubsection{\texorpdfstring{NadirAttitude()}{NadirAttitude()}\hspace{0.1cm}{\footnotesize\ttfamily [1/2]}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Nadir\+Attitude\+::\+Nadir\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Nadir\+Attitude\+::\+Nadir\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} @@ -47,11 +47,11 @@ {\em propagator} & \\ \hline \end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_af72bad35d416092ca326ca93906757c7}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_af72bad35d416092ca326ca93906757c7}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_aff17952207dcb51f47cc93fedb0b20fb}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1NadirAttitude_aff17952207dcb51f47cc93fedb0b20fb}} \index{IO::SDK::Maneuvers::Attitudes::NadirAttitude@{IO::SDK::Maneuvers::Attitudes::NadirAttitude}!NadirAttitude@{NadirAttitude}} \index{NadirAttitude@{NadirAttitude}!IO::SDK::Maneuvers::Attitudes::NadirAttitude@{IO::SDK::Maneuvers::Attitudes::NadirAttitude}} \doxysubsubsection{\texorpdfstring{NadirAttitude()}{NadirAttitude()}\hspace{0.1cm}{\footnotesize\ttfamily [2/2]}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Nadir\+Attitude\+::\+Nadir\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{minimum\+Epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Nadir\+Attitude\+::\+Nadir\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{minimum\+Epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} diff --git a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.pdf b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.pdf index 5128fcb2336f8154795f117727f4b1d5613db2b5..907c7effd2fc8c77631c5f2000ea7e6f941ede51 100644 GIT binary patch delta 200 zcmcbpe^GzKEFo?q^AJN5D^mk2W0T2Cg$z*m4}^B`TBatO8zm>F>KdCQT5et{Y{jHy zWNv6;YG7=lZD6EsV4$warSF@c;*waBs^MZ~WME`$Um*@6E0O%SARDy E0I#DmZvX%Q delta 200 zcmcbpe^GzKEFo?~%Me3TD-&}o1B=N^g$z*m4}^B`8XK9Ln5L!~=o+P(S!`Y^Y{jHy zXlZC_Vs2oeZD6EsV4$warSF@c;*waBs^MZ~WME`$Um*@6E0O%SARDy E09#HmyZ`_I diff --git a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.tex b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.tex index e658189e..68a6e422 100644 --- a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.tex +++ b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude.tex @@ -13,9 +13,9 @@ \doxysubsection*{Public Member Functions} \begin{DoxyCompactItemize} \item -\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a4befd3aa292dd8185e87c1f7b62f22c0}{Prograde\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) +\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a73af1392368d15c48ee2f892eef72f34}{Prograde\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) \begin{DoxyCompactList}\small\item\em Construct a new Prograde Attitude object. \end{DoxyCompactList}\item -\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_acfbcf91813954fb69de921837275049c}{Prograde\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&minimum\+Epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) +\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_ace2dd4a4221b2eb4cffae30ba6a4ee74}{Prograde\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&minimum\+Epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) \begin{DoxyCompactList}\small\item\em Construct a new Prograde Attitude object. \end{DoxyCompactList}\item bool \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_acc05df379c165ce5052799888f9e3719}{Can\+Execute}} (const \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO\+::\+SDK\+::\+Orbital\+Parameters\+::\+Orbital\+Parameters}} \&orbital\+Params) override \begin{DoxyCompactList}\small\item\em Evaluate if maneuver can occurs. \end{DoxyCompactList}\end{DoxyCompactItemize} @@ -30,11 +30,11 @@ \doxysubsection{Constructor \& Destructor Documentation} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a4befd3aa292dd8185e87c1f7b62f22c0}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a4befd3aa292dd8185e87c1f7b62f22c0}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a73af1392368d15c48ee2f892eef72f34}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_a73af1392368d15c48ee2f892eef72f34}} \index{IO::SDK::Maneuvers::Attitudes::ProgradeAttitude@{IO::SDK::Maneuvers::Attitudes::ProgradeAttitude}!ProgradeAttitude@{ProgradeAttitude}} \index{ProgradeAttitude@{ProgradeAttitude}!IO::SDK::Maneuvers::Attitudes::ProgradeAttitude@{IO::SDK::Maneuvers::Attitudes::ProgradeAttitude}} \doxysubsubsection{\texorpdfstring{ProgradeAttitude()}{ProgradeAttitude()}\hspace{0.1cm}{\footnotesize\ttfamily [1/2]}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Prograde\+Attitude\+::\+Prograde\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Prograde\+Attitude\+::\+Prograde\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} @@ -47,11 +47,11 @@ {\em propagator} & \\ \hline \end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_acfbcf91813954fb69de921837275049c}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_acfbcf91813954fb69de921837275049c}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_ace2dd4a4221b2eb4cffae30ba6a4ee74}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ProgradeAttitude_ace2dd4a4221b2eb4cffae30ba6a4ee74}} \index{IO::SDK::Maneuvers::Attitudes::ProgradeAttitude@{IO::SDK::Maneuvers::Attitudes::ProgradeAttitude}!ProgradeAttitude@{ProgradeAttitude}} \index{ProgradeAttitude@{ProgradeAttitude}!IO::SDK::Maneuvers::Attitudes::ProgradeAttitude@{IO::SDK::Maneuvers::Attitudes::ProgradeAttitude}} \doxysubsubsection{\texorpdfstring{ProgradeAttitude()}{ProgradeAttitude()}\hspace{0.1cm}{\footnotesize\ttfamily [2/2]}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Prograde\+Attitude\+::\+Prograde\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{minimum\+Epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Prograde\+Attitude\+::\+Prograde\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{minimum\+Epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} diff --git a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.pdf b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.pdf index e7e69c035b2930556ba73e4a0c45573d8c1f522e..e745df78c31a58885e2026da34aab8bff67d174c 100644 GIT binary patch delta 200 zcmcbpe^GzKEFo?q^AJN5D^mk2W0T2Cg$z*m4}^B`TBatO8zm>F>KdCQT5et{Y{jHy zWNv6;YG7=lZD6EsV4$warSF@c;*waBs^MZ~WME`$U#nKt5+ttL?)Y#J1!pPCh%+7|OidZf?JFeoA#G;alqSQ1lQ*#3oE>%@me>W}w D*NZa; delta 200 zcmcbpe^GzKEFo?~%Me3TD-&}o1B=N^g$z*m4}^B`8XK9Ln5L!~=o+P(S!`Y^Y{jHy zXlZC_Vs2oeZD6EsV4$warSF@c;*waBs^MZ~WME`$U+|0<) z$imqG$Tn~@G;}dGGBz@GHZ^cEva=zmB9_a}j;pvNv8be?C^e1C)ZD;?OI6j?-;E0Z DZ-O!Y diff --git a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.tex b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.tex index aa3a9dbe..156cca8e 100644 --- a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.tex +++ b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude.tex @@ -13,9 +13,9 @@ \doxysubsection*{Public Member Functions} \begin{DoxyCompactItemize} \item -\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a3867ab497cd0e694917d20e9d9a43334}{Retrograde\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) +\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a1c0f94622fa6b2c3641afe8a51da367b}{Retrograde\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) \begin{DoxyCompactList}\small\item\em Construct a new Retrograde Attitude object. \end{DoxyCompactList}\item -\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_add864c9248cf817e195e287acd8ed534}{Retrograde\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&minimum\+Epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) +\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a9e29a9c3846c15e59c11be42a47eb004}{Retrograde\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&minimum\+Epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) \begin{DoxyCompactList}\small\item\em Construct a new Retrograde Attitude object. \end{DoxyCompactList}\item bool \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_ace8726c7e00edf44bb790be5050a7f24}{Can\+Execute}} (const \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO\+::\+SDK\+::\+Orbital\+Parameters\+::\+Orbital\+Parameters}} \&orbital\+Params) override \begin{DoxyCompactList}\small\item\em Evaluate if maneuver can occurs. \end{DoxyCompactList}\end{DoxyCompactItemize} @@ -30,11 +30,11 @@ \doxysubsection{Constructor \& Destructor Documentation} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a3867ab497cd0e694917d20e9d9a43334}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a3867ab497cd0e694917d20e9d9a43334}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a1c0f94622fa6b2c3641afe8a51da367b}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a1c0f94622fa6b2c3641afe8a51da367b}} \index{IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude@{IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude}!RetrogradeAttitude@{RetrogradeAttitude}} \index{RetrogradeAttitude@{RetrogradeAttitude}!IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude@{IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude}} \doxysubsubsection{\texorpdfstring{RetrogradeAttitude()}{RetrogradeAttitude()}\hspace{0.1cm}{\footnotesize\ttfamily [1/2]}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Retrograde\+Attitude\+::\+Retrograde\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Retrograde\+Attitude\+::\+Retrograde\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} @@ -47,11 +47,11 @@ {\em propagator} & \\ \hline \end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_add864c9248cf817e195e287acd8ed534}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_add864c9248cf817e195e287acd8ed534}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a9e29a9c3846c15e59c11be42a47eb004}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1RetrogradeAttitude_a9e29a9c3846c15e59c11be42a47eb004}} \index{IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude@{IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude}!RetrogradeAttitude@{RetrogradeAttitude}} \index{RetrogradeAttitude@{RetrogradeAttitude}!IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude@{IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude}} \doxysubsubsection{\texorpdfstring{RetrogradeAttitude()}{RetrogradeAttitude()}\hspace{0.1cm}{\footnotesize\ttfamily [2/2]}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Retrograde\+Attitude\+::\+Retrograde\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{minimum\+Epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Retrograde\+Attitude\+::\+Retrograde\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{minimum\+Epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} diff --git a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.pdf b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.pdf index 700465e8f9206db9b2a445a598fbb085f91b6c59..f9bb193ab7483d25ca7021a7a2c3a2b5c73c62d0 100644 GIT binary patch delta 155 zcmbPjINNYTiZHj4d5EEjm8pT1vB~6oVFMKYD&ZZxmZ{0+M#;&ky2d7nmYefMte7~A z%neOU4S?!5ib=san=gyyFgjYAn3}<>k KsF>U!Aq@aieI~~M delta 155 zcmbPjINNYTiZHjKWr(4vm5I5PfyLx}VFMKYD&ZZx#zy8Qrm1NLx<;vH7Mt@$te7|q zEe%ag%z^4Rib=san=gyyFgltV8yOfGI~yAr85=uVS{fJ{S(;fIm|D7;nmC%7INRBn L5l}I?K|&e;4&o)^ diff --git a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.tex b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.tex index 9010dd80..ce217c83 100644 --- a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.tex +++ b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude.tex @@ -13,9 +13,9 @@ \doxysubsection*{Public Member Functions} \begin{DoxyCompactItemize} \item -\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a4f54adecfccb8b73e08a0bf8aef7dccb}{Toward\+Object\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration, const \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO\+::\+SDK\+::\+Body\+::\+Body}} \&target\+Body) +\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a6a1d2837006c792f1416441e4311c3ce}{Toward\+Object\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration, const \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO\+::\+SDK\+::\+Body\+::\+Body}} \&target\+Body) \begin{DoxyCompactList}\small\item\em Construct a new Toward Object Attitude object. \end{DoxyCompactList}\item -\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_aa55d17808cf7bdfef7ae703d985171d1}{Toward\+Object\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&minimum\+Epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration, const \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO\+::\+SDK\+::\+Body\+::\+Body}} \&target\+Body) +\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a5688038cc3a244c76b0bb8f53bd43b2b}{Toward\+Object\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&minimum\+Epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration, const \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO\+::\+SDK\+::\+Body\+::\+Body}} \&target\+Body) \begin{DoxyCompactList}\small\item\em Construct a new Toward Object Attitude object. \end{DoxyCompactList}\item bool \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a8d3620611d4b1983dfc2a15fbb9b1128}{Can\+Execute}} (const \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO\+::\+SDK\+::\+Orbital\+Parameters\+::\+Orbital\+Parameters}} \&orbital\+Params) override \begin{DoxyCompactList}\small\item\em Evaluate if maneuver can occurs. \end{DoxyCompactList}\end{DoxyCompactItemize} @@ -30,11 +30,11 @@ \doxysubsection{Constructor \& Destructor Documentation} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a4f54adecfccb8b73e08a0bf8aef7dccb}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a4f54adecfccb8b73e08a0bf8aef7dccb}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a6a1d2837006c792f1416441e4311c3ce}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a6a1d2837006c792f1416441e4311c3ce}} \index{IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude@{IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude}!TowardObjectAttitude@{TowardObjectAttitude}} \index{TowardObjectAttitude@{TowardObjectAttitude}!IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude@{IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude}} \doxysubsubsection{\texorpdfstring{TowardObjectAttitude()}{TowardObjectAttitude()}\hspace{0.1cm}{\footnotesize\ttfamily [1/2]}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Toward\+Object\+Attitude\+::\+Toward\+Object\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO\+::\+SDK\+::\+Body\+::\+Body}} \&}]{target\+Body }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Toward\+Object\+Attitude\+::\+Toward\+Object\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO\+::\+SDK\+::\+Body\+::\+Body}} \&}]{target\+Body }\end{DoxyParamCaption})} @@ -49,11 +49,11 @@ {\em target\+Body} & \\ \hline \end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_aa55d17808cf7bdfef7ae703d985171d1}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_aa55d17808cf7bdfef7ae703d985171d1}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a5688038cc3a244c76b0bb8f53bd43b2b}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1TowardObjectAttitude_a5688038cc3a244c76b0bb8f53bd43b2b}} \index{IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude@{IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude}!TowardObjectAttitude@{TowardObjectAttitude}} \index{TowardObjectAttitude@{TowardObjectAttitude}!IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude@{IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude}} \doxysubsubsection{\texorpdfstring{TowardObjectAttitude()}{TowardObjectAttitude()}\hspace{0.1cm}{\footnotesize\ttfamily [2/2]}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Toward\+Object\+Attitude\+::\+Toward\+Object\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{minimum\+Epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO\+::\+SDK\+::\+Body\+::\+Body}} \&}]{target\+Body }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Toward\+Object\+Attitude\+::\+Toward\+Object\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{minimum\+Epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Body}{IO\+::\+SDK\+::\+Body\+::\+Body}} \&}]{target\+Body }\end{DoxyParamCaption})} diff --git a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.pdf b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.pdf index 24ec9b6d7e3f784f682cb9d4deef974a0453afad..e32159d9b140c102a88b6c4115f2147d6992052f 100644 GIT binary patch delta 199 zcmeyU`%!npEKdCQT5dinWW}Uq zWNv6;YG7=tZD6EsV4$warSF@c;*waBs^MZ~WME`$U}&|Ch~=`g<0>vmEGnreN=@T3HL)<@QdM>JcjE#8 DbLcW1 delta 199 zcmeyU`%!npEjZ=11?onSARDy E0A2Mm4gdfE diff --git a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.tex b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.tex index 1bb72522..c6b1a7c9 100644 --- a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.tex +++ b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude.tex @@ -13,9 +13,9 @@ \doxysubsection*{Public Member Functions} \begin{DoxyCompactItemize} \item -\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a3dfe74492c2bed032f37ac4d02e153be}{Zenith\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) +\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a75359142c87e83ac94578e3b92242239}{Zenith\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) \begin{DoxyCompactList}\small\item\em Construct a new Zenith Attitude object. \end{DoxyCompactList}\item -\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a561ebd27bde3dd63d1e782ca35548fb6}{Zenith\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&minimum\+Epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) +\mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a1fd89c8b1e1a85f1b6bad1cdcd72410e}{Zenith\+Attitude}} (const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&engines, \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&propagator, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&minimum\+Epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&attitude\+Hold\+Duration) \begin{DoxyCompactList}\small\item\em Construct a new Zenith Attitude object. \end{DoxyCompactList}\item bool \mbox{\hyperlink{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a02199451b76c086541d3a99f5032ed84}{Can\+Execute}} (const \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters}{IO\+::\+SDK\+::\+Orbital\+Parameters\+::\+Orbital\+Parameters}} \&orbital\+Params) override \begin{DoxyCompactList}\small\item\em Evaluate if maneuver can occurs. \end{DoxyCompactList}\end{DoxyCompactItemize} @@ -30,11 +30,11 @@ \doxysubsection{Constructor \& Destructor Documentation} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a3dfe74492c2bed032f37ac4d02e153be}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a3dfe74492c2bed032f37ac4d02e153be}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a75359142c87e83ac94578e3b92242239}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a75359142c87e83ac94578e3b92242239}} \index{IO::SDK::Maneuvers::Attitudes::ZenithAttitude@{IO::SDK::Maneuvers::Attitudes::ZenithAttitude}!ZenithAttitude@{ZenithAttitude}} \index{ZenithAttitude@{ZenithAttitude}!IO::SDK::Maneuvers::Attitudes::ZenithAttitude@{IO::SDK::Maneuvers::Attitudes::ZenithAttitude}} \doxysubsubsection{\texorpdfstring{ZenithAttitude()}{ZenithAttitude()}\hspace{0.1cm}{\footnotesize\ttfamily [1/2]}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Zenith\+Attitude\+::\+Zenith\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Zenith\+Attitude\+::\+Zenith\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} @@ -47,11 +47,11 @@ {\em propagator} & \\ \hline \end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a561ebd27bde3dd63d1e782ca35548fb6}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a561ebd27bde3dd63d1e782ca35548fb6}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a1fd89c8b1e1a85f1b6bad1cdcd72410e}\label{classIO_1_1SDK_1_1Maneuvers_1_1Attitudes_1_1ZenithAttitude_a1fd89c8b1e1a85f1b6bad1cdcd72410e}} \index{IO::SDK::Maneuvers::Attitudes::ZenithAttitude@{IO::SDK::Maneuvers::Attitudes::ZenithAttitude}!ZenithAttitude@{ZenithAttitude}} \index{ZenithAttitude@{ZenithAttitude}!IO::SDK::Maneuvers::Attitudes::ZenithAttitude@{IO::SDK::Maneuvers::Attitudes::ZenithAttitude}} \doxysubsubsection{\texorpdfstring{ZenithAttitude()}{ZenithAttitude()}\hspace{0.1cm}{\footnotesize\ttfamily [2/2]}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Zenith\+Attitude\+::\+Zenith\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{minimum\+Epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Maneuvers\+::\+Attitudes\+::\+Zenith\+Attitude\+::\+Zenith\+Attitude (\begin{DoxyParamCaption}\item[{const std\+::vector$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1Spacecraft_1_1Engine}{IO\+::\+SDK\+::\+Body\+::\+Spacecraft\+::\+Engine}} $\ast$ $>$ \&}]{engines, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{IO\+::\+SDK\+::\+Propagators\+::\+Propagator}} \&}]{propagator, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{minimum\+Epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TimeSpan}{IO\+::\+SDK\+::\+Time\+::\+Time\+Span}} \&}]{attitude\+Hold\+Duration }\end{DoxyParamCaption})} diff --git a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver.pdf b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1CombinedManeuver.pdf index 079409be7fac80fcdf02b413c2bf4d20148c6cfb..0a2d2b7a82f40bcc18a69fb7f752438f070ab83e 100644 GIT binary patch delta 200 zcmcbpcTsPHln}R(d5EEjm8pT1vB_jrAp;bCg3u0L%hY6ZqvYgNU1O6(%gw67R!mw( z=7uJw2F51Z21e=z2I`tz`o8%oE{P?n8ZK5w21dpPrZ5$oJ4Le@V;v1mT#byKjf{*f z&0Wo0-OLTmjhsx3EsRV|TuhzZ%^a} E0Dn3#&j0`b delta 200 zcmcbpcTsPHln}R}Wr(4vm5I5Pf%#-rAp;bCg3u0LW5blBWD9cxU87Vpi_NOSR!mxk zmWHM#<_6~421e=z2I`tz`o8%oE{P?n8ZK5w21dpPrZ5$oJ4Le@V_n@W%q^Xa4NXi8 zjm=Gr%?!=VOw0{k44o~_TwP6_9PMlfs)*&Xv*Ri*Nh~U^a} E08h;@dH?_b diff --git a/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1ManeuverBase.pdf b/Docs/latex/classIO_1_1SDK_1_1Maneuvers_1_1ManeuverBase.pdf index 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-\mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_aa2ad5e93197a2465c3cf50b8065f6d61}{Orbital\+Parameters}} (const std\+::shared\+\_\+ptr$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1CelestialBody}{IO\+::\+SDK\+::\+Body\+::\+Celestial\+Body}} $>$ \¢er\+Of\+Motion, const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&epoch, const \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1Frames}{IO\+::\+SDK\+::\+Frames\+::\+Frames}} \&frame) +\mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_a2e151aad0e34a4bc0918f93ec536ea58}{Orbital\+Parameters}} (const std\+::shared\+\_\+ptr$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1CelestialBody}{IO\+::\+SDK\+::\+Body\+::\+Celestial\+Body}} $>$ \¢er\+Of\+Motion, \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} epoch, \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1Frames}{IO\+::\+SDK\+::\+Frames\+::\+Frames}} frame) \begin{DoxyCompactList}\small\item\em Construct a new Orbital \mbox{\hyperlink{namespaceIO_1_1SDK_1_1Parameters}{Parameters}} object. \end{DoxyCompactList}\item virtual \mbox{\hyperlink{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_a4c24cb357f03afe566885b46b86797c0}{$\sim$\+Orbital\+Parameters}} ()=default \item @@ -111,11 +111,11 @@ Orbital parameters. \doxysubsection{Constructor \& Destructor Documentation} -\mbox{\Hypertarget{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_aa2ad5e93197a2465c3cf50b8065f6d61}\label{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_aa2ad5e93197a2465c3cf50b8065f6d61}} +\mbox{\Hypertarget{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_a2e151aad0e34a4bc0918f93ec536ea58}\label{classIO_1_1SDK_1_1OrbitalParameters_1_1OrbitalParameters_a2e151aad0e34a4bc0918f93ec536ea58}} \index{IO::SDK::OrbitalParameters::OrbitalParameters@{IO::SDK::OrbitalParameters::OrbitalParameters}!OrbitalParameters@{OrbitalParameters}} \index{OrbitalParameters@{OrbitalParameters}!IO::SDK::OrbitalParameters::OrbitalParameters@{IO::SDK::OrbitalParameters::OrbitalParameters}} \doxysubsubsection{\texorpdfstring{OrbitalParameters()}{OrbitalParameters()}} -{\footnotesize\ttfamily IO\+::\+SDK\+::\+Orbital\+Parameters\+::\+Orbital\+Parameters\+::\+Orbital\+Parameters (\begin{DoxyParamCaption}\item[{const std\+::shared\+\_\+ptr$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1CelestialBody}{IO\+::\+SDK\+::\+Body\+::\+Celestial\+Body}} $>$ \&}]{center\+Of\+Motion, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}} \&}]{epoch, }\item[{const \mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1Frames}{IO\+::\+SDK\+::\+Frames\+::\+Frames}} \&}]{frame }\end{DoxyParamCaption})} +{\footnotesize\ttfamily IO\+::\+SDK\+::\+Orbital\+Parameters\+::\+Orbital\+Parameters\+::\+Orbital\+Parameters (\begin{DoxyParamCaption}\item[{const std\+::shared\+\_\+ptr$<$ \mbox{\hyperlink{classIO_1_1SDK_1_1Body_1_1CelestialBody}{IO\+::\+SDK\+::\+Body\+::\+Celestial\+Body}} $>$ \&}]{center\+Of\+Motion, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Time_1_1TDB}{IO\+::\+SDK\+::\+Time\+::\+TDB}}}]{epoch, }\item[{\mbox{\hyperlink{classIO_1_1SDK_1_1Frames_1_1Frames}{IO\+::\+SDK\+::\+Frames\+::\+Frames}}}]{frame }\end{DoxyParamCaption})} diff --git a/Docs/latex/classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector.pdf b/Docs/latex/classIO_1_1SDK_1_1OrbitalParameters_1_1StateVector.pdf index 69055aab84091fe0aec6ea18bcb968ba85236ef2..45e5e88dd45f284edf12ccdc657e1b90c7e47b9c 100644 GIT binary patch delta 156 zcmcbmeM@`8VgYU=^AJN5D^mk2W7Em&1PoC4F9mk+TBez%B^#Th>KdCQT5et^XvM@~ zWNv6;Y5-LKL0AgT*(@ZI&FExe>TFS*j}X6j^NW@c$%Y2jjG=4@zZ LLrBHs{i4zU1Uo1K delta 156 zcmcbmeM@`8VgYVL%Me3TD-&}o1B=P)1PoC4F9mk+8XK9Ln5L!~=o+P(S!`Y>XvM@~ zXlZC_Vh&XQL0AgT*(@ZI&FExgY~gC?Xku>WYGmeS=4j|*XkuYu>}=s?VPOWOE$wUw KshGT9R2l&5e<$ex diff --git a/Docs/latex/classIO_1_1SDK_1_1OrbitalParameters_1_1TLE.pdf b/Docs/latex/classIO_1_1SDK_1_1OrbitalParameters_1_1TLE.pdf index 16f8b941487be433d67122befb5b91838f999c6a..dcc730899cf3f682c944a03491656c856d0c9eaa 100644 GIT binary patch delta 156 zcmX@AeN=lxp8&U!d5EEjm8pT1vFYTQ0tP7jD*`)sEz?ZXl8sGLb&X9DEjP~;v|{2g zGB-3aH2|u=Ei47+Z2l{p&FExq;%aQ{Y-wq3Vrgn_W@ct=;B4ybWNB_;WMph)Xl`I)VPa@xVr*vWYGi0< LLrBHsRie@W)^I1O diff --git a/Docs/latex/classIO_1_1SDK_1_1Scenario.tex b/Docs/latex/classIO_1_1SDK_1_1Scenario.tex index 6af22cf9..5d8ec029 100644 --- a/Docs/latex/classIO_1_1SDK_1_1Scenario.tex +++ b/Docs/latex/classIO_1_1SDK_1_1Scenario.tex @@ -27,20 +27,6 @@ \item \mbox{\hyperlink{classIO_1_1SDK_1_1Propagators_1_1Propagator}{Propagators\+::\+Propagator}} \& \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_aeee297b71c3a8eeabdf538e24ad7182a}{Get\+Propagator}} () \item -void \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a1edecc4b70536953805561cfcb6f263f}{Add\+Distance\+Constraint}} (Constraints\+::\+Parameters\+::\+Distance\+Parameters $\ast$distance\+Parameters) -\item -void \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_ad90005ecbd0ec3bf596c81e4758023d7}{Add\+Occultation\+Constraint}} (IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+Occultation\+Parameters $\ast$occultation\+Parameters) -\item -void \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_ac87ca28b5c56abea86b626a6067e9e03}{Add\+Day\+Constraint}} (IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+By\+Day\+Parameters $\ast$by\+Day\+Parameters) -\item -void \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_aefd1fe0c77211b597e71599be8f8482a}{Add\+Night\+Constraint}} (IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+By\+Night\+Parameters $\ast$by\+Night\+Parameters) -\item -void \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a38fb82b4679d789a253bcfa29ef627d4}{Add\+Body\+Visibility\+Constraint}} (IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+Body\+Visibility\+From\+Site\+Parameters $\ast$body\+Visibility\+Parameters) -\item -void \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a0e3cd3bf3d3e6a238cf2c69ced4b922e}{Add\+In\+Field\+Of\+View\+Constraint}} (IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+In\+Field\+Of\+View\+Parameters $\ast$in\+Field\+Of\+View\+Parameters) -\item -void \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a48c2803d92a0487167a9490dc75c4aac}{Add\+Launch\+Constraint}} (IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+Launch\+Parameters $\ast$launch\+Parameters) -\item void \mbox{\hyperlink{classIO_1_1SDK_1_1Scenario_a5023a3fec59ef54ca3d1f301d8313d19}{Execute}} () \end{DoxyCompactItemize} @@ -55,17 +41,6 @@ \doxysubsection{Member Function Documentation} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_a38fb82b4679d789a253bcfa29ef627d4}\label{classIO_1_1SDK_1_1Scenario_a38fb82b4679d789a253bcfa29ef627d4}} -\index{IO::SDK::Scenario@{IO::SDK::Scenario}!AddBodyVisibilityConstraint@{AddBodyVisibilityConstraint}} -\index{AddBodyVisibilityConstraint@{AddBodyVisibilityConstraint}!IO::SDK::Scenario@{IO::SDK::Scenario}} -\doxysubsubsection{\texorpdfstring{AddBodyVisibilityConstraint()}{AddBodyVisibilityConstraint()}} -{\footnotesize\ttfamily void IO\+::\+SDK\+::\+Scenario\+::\+Add\+Body\+Visibility\+Constraint (\begin{DoxyParamCaption}\item[{IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+Body\+Visibility\+From\+Site\+Parameters $\ast$}]{body\+Visibility\+Parameters }\end{DoxyParamCaption})} - -Add a body visibility constraint -\begin{DoxyParams}{Parameters} -{\em body\+Visibility\+Parameters} & \\ -\hline -\end{DoxyParams} \mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_a786a1044cf68de4ecc85aef250f01eba}\label{classIO_1_1SDK_1_1Scenario_a786a1044cf68de4ecc85aef250f01eba}} \index{IO::SDK::Scenario@{IO::SDK::Scenario}!AddCelestialBody@{AddCelestialBody}} \index{AddCelestialBody@{AddCelestialBody}!IO::SDK::Scenario@{IO::SDK::Scenario}} @@ -77,72 +52,6 @@ {\em celestial\+Body} & \\ \hline \end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_ac87ca28b5c56abea86b626a6067e9e03}\label{classIO_1_1SDK_1_1Scenario_ac87ca28b5c56abea86b626a6067e9e03}} -\index{IO::SDK::Scenario@{IO::SDK::Scenario}!AddDayConstraint@{AddDayConstraint}} -\index{AddDayConstraint@{AddDayConstraint}!IO::SDK::Scenario@{IO::SDK::Scenario}} -\doxysubsubsection{\texorpdfstring{AddDayConstraint()}{AddDayConstraint()}} -{\footnotesize\ttfamily void IO\+::\+SDK\+::\+Scenario\+::\+Add\+Day\+Constraint (\begin{DoxyParamCaption}\item[{IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+By\+Day\+Parameters $\ast$}]{by\+Day\+Parameters }\end{DoxyParamCaption})} - -Add a day constraint -\begin{DoxyParams}{Parameters} -{\em by\+Day\+Parameters} & \\ -\hline -\end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_a1edecc4b70536953805561cfcb6f263f}\label{classIO_1_1SDK_1_1Scenario_a1edecc4b70536953805561cfcb6f263f}} -\index{IO::SDK::Scenario@{IO::SDK::Scenario}!AddDistanceConstraint@{AddDistanceConstraint}} -\index{AddDistanceConstraint@{AddDistanceConstraint}!IO::SDK::Scenario@{IO::SDK::Scenario}} -\doxysubsubsection{\texorpdfstring{AddDistanceConstraint()}{AddDistanceConstraint()}} -{\footnotesize\ttfamily void IO\+::\+SDK\+::\+Scenario\+::\+Add\+Distance\+Constraint (\begin{DoxyParamCaption}\item[{Constraints\+::\+Parameters\+::\+Distance\+Parameters $\ast$}]{distance\+Parameters }\end{DoxyParamCaption})} - -Add a distance constraint -\begin{DoxyParams}{Parameters} -{\em distance\+Parameters} & \\ -\hline -\end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_a0e3cd3bf3d3e6a238cf2c69ced4b922e}\label{classIO_1_1SDK_1_1Scenario_a0e3cd3bf3d3e6a238cf2c69ced4b922e}} -\index{IO::SDK::Scenario@{IO::SDK::Scenario}!AddInFieldOfViewConstraint@{AddInFieldOfViewConstraint}} -\index{AddInFieldOfViewConstraint@{AddInFieldOfViewConstraint}!IO::SDK::Scenario@{IO::SDK::Scenario}} -\doxysubsubsection{\texorpdfstring{AddInFieldOfViewConstraint()}{AddInFieldOfViewConstraint()}} -{\footnotesize\ttfamily void IO\+::\+SDK\+::\+Scenario\+::\+Add\+In\+Field\+Of\+View\+Constraint (\begin{DoxyParamCaption}\item[{IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+In\+Field\+Of\+View\+Parameters $\ast$}]{in\+Field\+Of\+View\+Parameters }\end{DoxyParamCaption})} - -Add a field of view constraint -\begin{DoxyParams}{Parameters} -{\em in\+Field\+Of\+View\+Parameters} & \\ -\hline -\end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_a48c2803d92a0487167a9490dc75c4aac}\label{classIO_1_1SDK_1_1Scenario_a48c2803d92a0487167a9490dc75c4aac}} -\index{IO::SDK::Scenario@{IO::SDK::Scenario}!AddLaunchConstraint@{AddLaunchConstraint}} -\index{AddLaunchConstraint@{AddLaunchConstraint}!IO::SDK::Scenario@{IO::SDK::Scenario}} -\doxysubsubsection{\texorpdfstring{AddLaunchConstraint()}{AddLaunchConstraint()}} -{\footnotesize\ttfamily void IO\+::\+SDK\+::\+Scenario\+::\+Add\+Launch\+Constraint (\begin{DoxyParamCaption}\item[{IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+Launch\+Parameters $\ast$}]{launch\+Parameters }\end{DoxyParamCaption})} - -Add launch constraint -\begin{DoxyParams}{Parameters} -{\em launch\+Parameters} & \\ -\hline -\end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_aefd1fe0c77211b597e71599be8f8482a}\label{classIO_1_1SDK_1_1Scenario_aefd1fe0c77211b597e71599be8f8482a}} -\index{IO::SDK::Scenario@{IO::SDK::Scenario}!AddNightConstraint@{AddNightConstraint}} -\index{AddNightConstraint@{AddNightConstraint}!IO::SDK::Scenario@{IO::SDK::Scenario}} -\doxysubsubsection{\texorpdfstring{AddNightConstraint()}{AddNightConstraint()}} -{\footnotesize\ttfamily void IO\+::\+SDK\+::\+Scenario\+::\+Add\+Night\+Constraint (\begin{DoxyParamCaption}\item[{IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+By\+Night\+Parameters $\ast$}]{by\+Night\+Parameters }\end{DoxyParamCaption})} - -Add a night constraint -\begin{DoxyParams}{Parameters} -{\em by\+Night\+Parameters} & \\ -\hline -\end{DoxyParams} -\mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_ad90005ecbd0ec3bf596c81e4758023d7}\label{classIO_1_1SDK_1_1Scenario_ad90005ecbd0ec3bf596c81e4758023d7}} -\index{IO::SDK::Scenario@{IO::SDK::Scenario}!AddOccultationConstraint@{AddOccultationConstraint}} -\index{AddOccultationConstraint@{AddOccultationConstraint}!IO::SDK::Scenario@{IO::SDK::Scenario}} -\doxysubsubsection{\texorpdfstring{AddOccultationConstraint()}{AddOccultationConstraint()}} -{\footnotesize\ttfamily void IO\+::\+SDK\+::\+Scenario\+::\+Add\+Occultation\+Constraint (\begin{DoxyParamCaption}\item[{IO\+::\+SDK\+::\+Constraints\+::\+Parameters\+::\+Occultation\+Parameters $\ast$}]{occultation\+Parameters }\end{DoxyParamCaption})} - -Add an occultation constraint -\begin{DoxyParams}{Parameters} -{\em occultation\+Parameters} & \\ -\hline -\end{DoxyParams} \mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_a8468e291b7910ec50fab34035bf1e178}\label{classIO_1_1SDK_1_1Scenario_a8468e291b7910ec50fab34035bf1e178}} \index{IO::SDK::Scenario@{IO::SDK::Scenario}!AddSite@{AddSite}} \index{AddSite@{AddSite}!IO::SDK::Scenario@{IO::SDK::Scenario}} @@ -171,7 +80,7 @@ \doxysubsubsection{\texorpdfstring{Execute()}{Execute()}} {\footnotesize\ttfamily void IO\+::\+SDK\+::\+Scenario\+::\+Execute (\begin{DoxyParamCaption}{ }\end{DoxyParamCaption})} -Execute scenario, propagate spacecrafts, simulate maneuvers, evaluate constraints \mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_a6544f3a19931cd174f2f2c811d8fdf4c}\label{classIO_1_1SDK_1_1Scenario_a6544f3a19931cd174f2f2c811d8fdf4c}} +Execute scenario \mbox{\Hypertarget{classIO_1_1SDK_1_1Scenario_a6544f3a19931cd174f2f2c811d8fdf4c}\label{classIO_1_1SDK_1_1Scenario_a6544f3a19931cd174f2f2c811d8fdf4c}} \index{IO::SDK::Scenario@{IO::SDK::Scenario}!GetCelestialBodies@{GetCelestialBodies}} 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\mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a37aaff67723471afe0b424b1c5f45b62}{serial\+Number}} +const char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_aaaef37ff022681b8c013aabc22cf6bd3}{serial\+Number}} \item -char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a57fb452f92b221d0628df58fcec099dd}{fuel\+Tank\+Serial\+Number}} +const char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_ae1586be547c6c629ef9fffa48ce3eb3e}{fuel\+Tank\+Serial\+Number}} \item -char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a8eba4c4ea41e59883a38b5b31fc0c1cd}{name}} +const char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_afba82457c3dba1f96881de6c7f96c6fc}{name}} \item double \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a0ff30313e1775ad5bfcf6c290597bb83}{isp}} \item -double \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a9a295704e9d53487bbbb3d11fc5e99e8}{fuelflow}} +double \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_acb4c6108c1622e33f4b016ac6e933fe6}{fuel\+Flow}} \end{DoxyCompactItemize} \doxysubsection{Member Data Documentation} -\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a9a295704e9d53487bbbb3d11fc5e99e8}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a9a295704e9d53487bbbb3d11fc5e99e8}} -\index{IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}!fuelflow@{fuelflow}} -\index{fuelflow@{fuelflow}!IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}} -\doxysubsubsection{\texorpdfstring{fuelflow}{fuelflow}} -{\footnotesize\ttfamily double IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Engine\+DTO\+::fuelflow} +\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_acb4c6108c1622e33f4b016ac6e933fe6}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_acb4c6108c1622e33f4b016ac6e933fe6}} +\index{IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}!fuelFlow@{fuelFlow}} +\index{fuelFlow@{fuelFlow}!IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}} +\doxysubsubsection{\texorpdfstring{fuelFlow}{fuelFlow}} +{\footnotesize\ttfamily double IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Engine\+DTO\+::fuel\+Flow} -\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a57fb452f92b221d0628df58fcec099dd}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a57fb452f92b221d0628df58fcec099dd}} +\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_ae1586be547c6c629ef9fffa48ce3eb3e}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_ae1586be547c6c629ef9fffa48ce3eb3e}} \index{IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}!fuelTankSerialNumber@{fuelTankSerialNumber}} \index{fuelTankSerialNumber@{fuelTankSerialNumber}!IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}} \doxysubsubsection{\texorpdfstring{fuelTankSerialNumber}{fuelTankSerialNumber}} -{\footnotesize\ttfamily char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Engine\+DTO\+::fuel\+Tank\+Serial\+Number} +{\footnotesize\ttfamily const char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Engine\+DTO\+::fuel\+Tank\+Serial\+Number} \mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_ae946e724e129f39d66841a6c60fb357f}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_ae946e724e129f39d66841a6c60fb357f}} \index{IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}!id@{id}} @@ -46,17 +46,17 @@ \doxysubsubsection{\texorpdfstring{isp}{isp}} {\footnotesize\ttfamily double IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Engine\+DTO\+::isp} -\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a8eba4c4ea41e59883a38b5b31fc0c1cd}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a8eba4c4ea41e59883a38b5b31fc0c1cd}} +\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_afba82457c3dba1f96881de6c7f96c6fc}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_afba82457c3dba1f96881de6c7f96c6fc}} \index{IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}!name@{name}} \index{name@{name}!IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}} \doxysubsubsection{\texorpdfstring{name}{name}} -{\footnotesize\ttfamily char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Engine\+DTO\+::name} +{\footnotesize\ttfamily const char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Engine\+DTO\+::name} -\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a37aaff67723471afe0b424b1c5f45b62}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_a37aaff67723471afe0b424b1c5f45b62}} +\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_aaaef37ff022681b8c013aabc22cf6bd3}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1EngineDTO_aaaef37ff022681b8c013aabc22cf6bd3}} \index{IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}!serialNumber@{serialNumber}} \index{serialNumber@{serialNumber}!IO::SDK::API::DTO::EngineDTO@{IO::SDK::API::DTO::EngineDTO}} \doxysubsubsection{\texorpdfstring{serialNumber}{serialNumber}} -{\footnotesize\ttfamily char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Engine\+DTO\+::serial\+Number} +{\footnotesize\ttfamily const char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Engine\+DTO\+::serial\+Number} diff --git a/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.tex b/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.tex index fc6a6030..18f7815b 100644 --- a/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.tex +++ b/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO.tex @@ -9,7 +9,7 @@ \item int \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_ad511fe1e6898cc0280b0069f1f44207e}{id}} \item -char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_ad8aa5e4becba2f0767fa310849b8f1a1}{serial\+Number}} +const char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_a52f3d0b45205f9b3e84f0bce316abe91}{serial\+Number}} \item double \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_aa8d92790c4185a373b2c013a2bb816ed}{capacity}} \item @@ -36,11 +36,11 @@ \doxysubsubsection{\texorpdfstring{quantity}{quantity}} {\footnotesize\ttfamily double IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Fuel\+Tank\+DTO\+::quantity} -\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_ad8aa5e4becba2f0767fa310849b8f1a1}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_ad8aa5e4becba2f0767fa310849b8f1a1}} +\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_a52f3d0b45205f9b3e84f0bce316abe91}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1FuelTankDTO_a52f3d0b45205f9b3e84f0bce316abe91}} \index{IO::SDK::API::DTO::FuelTankDTO@{IO::SDK::API::DTO::FuelTankDTO}!serialNumber@{serialNumber}} \index{serialNumber@{serialNumber}!IO::SDK::API::DTO::FuelTankDTO@{IO::SDK::API::DTO::FuelTankDTO}} \doxysubsubsection{\texorpdfstring{serialNumber}{serialNumber}} -{\footnotesize\ttfamily char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Fuel\+Tank\+DTO\+::serial\+Number} +{\footnotesize\ttfamily const char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Fuel\+Tank\+DTO\+::serial\+Number} diff --git a/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.tex b/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.tex index 127907dd..775a9b95 100644 --- a/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.tex +++ b/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO.tex @@ -9,7 +9,7 @@ \item int \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_a8c9d63e641f8ec865cc7c8e7369b0f3a}{maneuver\+Order}} \{-\/1\} \item -char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ac92b335a51002a99f037eaf11fe0cf1c}{engines}} \mbox{[}5\mbox{]} \{\} +const char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ac68a3c6f143c4e2468ddeb1d6d091e99}{engines}} \mbox{[}5\mbox{]} \{\} \item double \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ae949350a0a86deccbc35378e75a73e80}{attitude\+Hold\+Duration}} \{0.\+0\} \item @@ -48,11 +48,11 @@ \doxysubsubsection{\texorpdfstring{deltaV}{deltaV}} {\footnotesize\ttfamily \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1Vector3DDTO}{Vector3\+DDTO}} IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Orbital\+Plane\+Changing\+Maneuver\+DTO\+::deltaV \{\}} -\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ac92b335a51002a99f037eaf11fe0cf1c}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ac92b335a51002a99f037eaf11fe0cf1c}} +\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ac68a3c6f143c4e2468ddeb1d6d091e99}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_ac68a3c6f143c4e2468ddeb1d6d091e99}} \index{IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO@{IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO}!engines@{engines}} \index{engines@{engines}!IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO@{IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO}} \doxysubsubsection{\texorpdfstring{engines}{engines}} -{\footnotesize\ttfamily char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Orbital\+Plane\+Changing\+Maneuver\+DTO\+::engines\mbox{[}5\mbox{]} \{\}} +{\footnotesize\ttfamily const char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Orbital\+Plane\+Changing\+Maneuver\+DTO\+::engines\mbox{[}5\mbox{]} \{\}} \mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_a3e3483a71116f130eb080c7e7819905f}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1OrbitalPlaneChangingManeuverDTO_a3e3483a71116f130eb080c7e7819905f}} \index{IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO@{IO::SDK::API::DTO::OrbitalPlaneChangingManeuverDTO}!FuelBurned@{FuelBurned}} diff --git a/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.tex b/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.tex index 842a697b..c2517b48 100644 --- a/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.tex +++ b/Docs/latex/structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO.tex @@ -7,7 +7,7 @@ \doxysubsection*{Public Attributes} \begin{DoxyCompactItemize} \item -char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a46fecef09b2136f0d48b606cd0026430}{Name}} \{\} +const char $\ast$ \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a19b9d3b85ddcc93df6029ea267ab1a85}{Name}} \{\} \item \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1WindowDTO}{Window\+DTO}} \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a36715d36708f0c714a8f6cdcfc232ad6}{Window}} \{\} \item @@ -26,11 +26,11 @@ \doxysubsubsection{\texorpdfstring{CelestialBodies}{CelestialBodies}} {\footnotesize\ttfamily \mbox{\hyperlink{structIO_1_1SDK_1_1API_1_1DTO_1_1CelestialBodyDTO}{Celestial\+Body\+DTO}} IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Scenario\+DTO\+::\+Celestial\+Bodies\mbox{[}10\mbox{]}} -\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a46fecef09b2136f0d48b606cd0026430}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a46fecef09b2136f0d48b606cd0026430}} +\mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a19b9d3b85ddcc93df6029ea267ab1a85}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a19b9d3b85ddcc93df6029ea267ab1a85}} \index{IO::SDK::API::DTO::ScenarioDTO@{IO::SDK::API::DTO::ScenarioDTO}!Name@{Name}} \index{Name@{Name}!IO::SDK::API::DTO::ScenarioDTO@{IO::SDK::API::DTO::ScenarioDTO}} \doxysubsubsection{\texorpdfstring{Name}{Name}} -{\footnotesize\ttfamily char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Scenario\+DTO\+::\+Name \{\}} +{\footnotesize\ttfamily const char$\ast$ IO\+::\+SDK\+::\+API\+::\+DTO\+::\+Scenario\+DTO\+::\+Name \{\}} \mbox{\Hypertarget{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a232567cfa43075df51e869cd26d659cb}\label{structIO_1_1SDK_1_1API_1_1DTO_1_1ScenarioDTO_a232567cfa43075df51e869cd26d659cb}} \index{IO::SDK::API::DTO::ScenarioDTO@{IO::SDK::API::DTO::ScenarioDTO}!Sites@{Sites}} diff --git a/IO.SDK.Tests/APITests.cpp b/IO.SDK.Tests/APITests.cpp index 40c01409..197a5597 100644 --- a/IO.SDK.Tests/APITests.cpp +++ b/IO.SDK.Tests/APITests.cpp @@ -102,7 +102,7 @@ TEST(API, SpacecraftPropagation) scenario.Spacecraft.engines[0].name = "eng1"; scenario.Spacecraft.engines[0].serialNumber = "eng1"; scenario.Spacecraft.engines[0].fuelTankSerialNumber = "ft1"; - scenario.Spacecraft.engines[0].fuelflow = 50.0; + scenario.Spacecraft.engines[0].fuelFlow = 50.0; scenario.Spacecraft.engines[0].isp = 450.0; scenario.Spacecraft.payloads[0].serialNumber = "pl1"; @@ -215,7 +215,6 @@ TEST(API, FindWindowsInFieldOfViewConstraintProxy) std::move(orbitalParams)}; s.AddCircularFOVInstrument(789, "CAMERA789", orientation, boresight, fovvector, 1.5); - const IO::SDK::Instruments::Instrument *instrument{s.GetInstrument(789)}; //==========PROPAGATOR==================== auto step{IO::SDK::Time::TimeSpan(1.0s)}; diff --git a/IO.SDK/API/DTO/EngineDTO.h b/IO.SDK/API/DTO/EngineDTO.h index cb361877..1961a009 100644 --- a/IO.SDK/API/DTO/EngineDTO.h +++ b/IO.SDK/API/DTO/EngineDTO.h @@ -5,11 +5,11 @@ namespace IO::SDK::API::DTO struct EngineDTO { int id; - char * serialNumber; - char * fuelTankSerialNumber; - char * name; + const char * serialNumber; + const char * fuelTankSerialNumber; + const char * name; double isp; - double fuelflow; + double fuelFlow; }; } \ No newline at end of file diff --git a/IO.SDK/API/DTO/FuelTankDTO.h b/IO.SDK/API/DTO/FuelTankDTO.h index 6723f831..64efb3ef 100644 --- a/IO.SDK/API/DTO/FuelTankDTO.h +++ b/IO.SDK/API/DTO/FuelTankDTO.h @@ -5,7 +5,7 @@ namespace IO::SDK::API::DTO struct FuelTankDTO { int id; - char * serialNumber; + const char * serialNumber; double capacity; double quantity; diff --git a/IO.SDK/API/DTO/OrbitalPlaneChangingManeuverDTO.h b/IO.SDK/API/DTO/OrbitalPlaneChangingManeuverDTO.h index 277b5e0a..def889c8 100644 --- a/IO.SDK/API/DTO/OrbitalPlaneChangingManeuverDTO.h +++ b/IO.SDK/API/DTO/OrbitalPlaneChangingManeuverDTO.h @@ -13,7 +13,7 @@ namespace IO::SDK::API::DTO struct OrbitalPlaneChangingManeuverDTO { int maneuverOrder{-1}; - char* engines[5]{}; + const char* engines[5]{}; double attitudeHoldDuration{0.0}; double minimumEpoch{0.0}; diff --git a/IO.SDK/API/DTO/ScenarioDTO.h b/IO.SDK/API/DTO/ScenarioDTO.h index 930848b7..2ebe0e4d 100644 --- a/IO.SDK/API/DTO/ScenarioDTO.h +++ b/IO.SDK/API/DTO/ScenarioDTO.h @@ -9,7 +9,7 @@ namespace IO::SDK::API::DTO { struct ScenarioDTO { - char *Name{}; + const char *Name{}; WindowDTO Window{}; SpacecraftDTO Spacecraft; SiteDTO Sites[10]; diff --git a/IO.SDK/API/Proxy.cpp b/IO.SDK/API/Proxy.cpp index bd4a9435..74184a68 100644 --- a/IO.SDK/API/Proxy.cpp +++ b/IO.SDK/API/Proxy.cpp @@ -630,7 +630,7 @@ void BuildEngines(const IO::SDK::API::DTO::ScenarioDTO &scenarioDto, } spacecraft.AddEngine(engine.serialNumber, engine.name, engine.fuelTankSerialNumber, IO::SDK::Math::Vector3D::Zero, IO::SDK::Math::Vector3D::Zero, engine.isp, - engine.fuelflow); + engine.fuelFlow); } } diff --git a/IO.SDK/API/Proxy.h b/IO.SDK/API/Proxy.h index 3b199346..880ae5bb 100644 --- a/IO.SDK/API/Proxy.h +++ b/IO.SDK/API/Proxy.h @@ -216,7 +216,7 @@ MODULE_API IO::SDK::API::DTO::CelestialBodyDTO GetCelestialBodyInfoProxy(int bod #ifdef __cplusplus } #endif -#pragma endregion +#pragma endregion Proxy #ifndef PROXY_H #define PROXY_H diff --git a/IO.SDK/Body/Body.cpp b/IO.SDK/Body/Body.cpp index fd32ebd3..bc91cc1d 100644 --- a/IO.SDK/Body/Body.cpp +++ b/IO.SDK/Body/Body.cpp @@ -136,7 +136,7 @@ IO::SDK::Body::Body::FindWindowsOnOccultationConstraint(const IO::SDK::Time::Win { std::string bshape{"POINT"}; std::string bframe{}; - auto selectedOccultation = OccultationType::Any(); + auto selectedOccultation {OccultationType::Any()}; if (IO::SDK::Helpers::IsInstanceOf(&targetBody)) { bshape = "ELLIPSOID"; diff --git a/IO.SDK/Body/Spacecraft/Spacecraft.h b/IO.SDK/Body/Spacecraft/Spacecraft.h index 0493ecc0..f79d916c 100644 --- a/IO.SDK/Body/Spacecraft/Spacecraft.h +++ b/IO.SDK/Body/Spacecraft/Spacecraft.h @@ -341,7 +341,7 @@ namespace IO::SDK::Body::Spacecraft */ const std::unique_ptr &GetFrame() const; - inline double GetMaximumOperatingMass() + inline double GetMaximumOperatingMass() const { return m_maximumOperatingMass; } }; } diff --git a/IO.SDK/Constraints/GeometryFinder.cpp b/IO.SDK/Constraints/GeometryFinder.cpp index ef84e6ab..87a661e6 100644 --- a/IO.SDK/Constraints/GeometryFinder.cpp +++ b/IO.SDK/Constraints/GeometryFinder.cpp @@ -5,9 +5,7 @@ #include #include #include -#include "CelestialBody.h" #include "IlluminationAngle.h" -#include std::vector> IO::SDK::Constraints::GeometryFinder::FindWindowsOnDistanceConstraint(const IO::SDK::Time::Window &searchWindow, int observerId, diff --git a/IO.SDK/Constraints/RelationnalOperator.cpp b/IO.SDK/Constraints/RelationnalOperator.cpp index a639a344..67c07fe2 100644 --- a/IO.SDK/Constraints/RelationnalOperator.cpp +++ b/IO.SDK/Constraints/RelationnalOperator.cpp @@ -11,7 +11,6 @@ #include "RelationalOperator.h" #include -#include #include IO::SDK::Constraints::RelationalOperator IO::SDK::Constraints::RelationalOperator::mGreaterThan(std::string(">")); diff --git a/IO.SDK/Coordinate.cpp b/IO.SDK/Coordinate.cpp index 4817c233..ff1cfb73 100644 --- a/IO.SDK/Coordinate.cpp +++ b/IO.SDK/Coordinate.cpp @@ -9,6 +9,8 @@ * */ #include + +#include #include "SDKException.h" IO::SDK::Coordinate IO::SDK::Coordinate::mX(std::string("X")); @@ -23,7 +25,7 @@ IO::SDK::Coordinate IO::SDK::Coordinate::mRadius(std::string("RADIUS")); IO::SDK::Coordinate IO::SDK::Coordinate::mRange(std::string("RANGE")); IO::SDK::Coordinate IO::SDK::Coordinate::mRightAscension(std::string("RIGHT ASCENSION")); -IO::SDK::Coordinate::Coordinate(const std::string &name) : m_name{name} +IO::SDK::Coordinate::Coordinate(std::string name) : m_name{std::move(name)} { } @@ -87,7 +89,7 @@ IO::SDK::Coordinate &IO::SDK::Coordinate::Colatitude() return mColatitude; } -IO::SDK::Coordinate IO::SDK::Coordinate::ToCoordinateType(const std::string &coordinateType) +IO::SDK::Coordinate& IO::SDK::Coordinate::ToCoordinateType(const std::string &coordinateType) { if (coordinateType == Coordinate::mAltitude.ToCharArray()) { diff --git a/IO.SDK/Coordinate.h b/IO.SDK/Coordinate.h index 24f4b607..cfc19e5c 100644 --- a/IO.SDK/Coordinate.h +++ b/IO.SDK/Coordinate.h @@ -39,7 +39,7 @@ namespace IO::SDK * * @param name */ - explicit Coordinate(const std::string &name); + explicit Coordinate(std::string name); ~Coordinate() = default; Coordinate &operator=(const Coordinate &other) @@ -70,7 +70,7 @@ namespace IO::SDK static Coordinate& RightAscension(); static Coordinate& Declination(); static Coordinate& Colatitude(); - static Coordinate ToCoordinateType(const std::string &coordinateType) ; + static Coordinate& ToCoordinateType(const std::string &coordinateType) ; }; } // namespace IO::SDK diff --git a/IO.SDK/Frames/FrameFile.cpp b/IO.SDK/Frames/FrameFile.cpp index 8945016b..247c520f 100644 --- a/IO.SDK/Frames/FrameFile.cpp +++ b/IO.SDK/Frames/FrameFile.cpp @@ -10,9 +10,10 @@ */ #include #include +#include #include -IO::SDK::Frames::FrameFile::FrameFile(const std::string& filePath, const std::string& name) : m_filePath{ filePath }, m_name{ name } +IO::SDK::Frames::FrameFile::FrameFile(const std::string& filePath, std::string name) : m_filePath{ filePath }, m_name{std::move( name )} { auto directory = std::filesystem::directory_entry(filePath).path(); if (directory.has_parent_path()) diff --git a/IO.SDK/Frames/FrameFile.h b/IO.SDK/Frames/FrameFile.h index 9884cab3..37da951a 100644 --- a/IO.SDK/Frames/FrameFile.h +++ b/IO.SDK/Frames/FrameFile.h @@ -26,7 +26,7 @@ namespace IO::SDK::Frames const std::string m_filePath{}; bool m_fileExists{ false }; bool m_isLoaded{ false }; - FrameFile(const std::string& filePath, const std::string& name); + FrameFile(const std::string& filePath, std::string name); const std::string m_name{}; public: diff --git a/IO.SDK/Kernels/SpacecraftClockKernel.cpp b/IO.SDK/Kernels/SpacecraftClockKernel.cpp index de600700..8c388fa7 100644 --- a/IO.SDK/Kernels/SpacecraftClockKernel.cpp +++ b/IO.SDK/Kernels/SpacecraftClockKernel.cpp @@ -116,7 +116,7 @@ double IO::SDK::Kernels::SpacecraftClockKernel::ConvertToEncodedClock(const IO:: int IO::SDK::Kernels::SpacecraftClockKernel::GetTicksPerSeconds() const { - return std::pow(2.0, m_resolution); + return std::pow(2, m_resolution); } double IO::SDK::Kernels::SpacecraftClockKernel::GetSecondsPerTick() const diff --git a/IO.SDK/Maneuvers/ApogeeHeightChangingManeuver.cpp b/IO.SDK/Maneuvers/ApogeeHeightChangingManeuver.cpp index 7afca9c4..93d1c601 100644 --- a/IO.SDK/Maneuvers/ApogeeHeightChangingManeuver.cpp +++ b/IO.SDK/Maneuvers/ApogeeHeightChangingManeuver.cpp @@ -10,13 +10,14 @@ */ #include #include +#include #include -IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::ApogeeHeightChangingManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, const double targetHeight) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator), m_targetHeight{targetHeight} +IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::ApogeeHeightChangingManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, const double targetHeight) : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator), m_targetHeight{targetHeight} { } -IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::ApogeeHeightChangingManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, const double targetHeight, const IO::SDK::Time::TDB &minimumEpoch) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, minimumEpoch), m_targetHeight{targetHeight} +IO::SDK::Maneuvers::ApogeeHeightChangingManeuver::ApogeeHeightChangingManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, const double targetHeight, const IO::SDK::Time::TDB &minimumEpoch) : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator, minimumEpoch), m_targetHeight{targetHeight} { } diff --git a/IO.SDK/Maneuvers/ApsidalAlignmentManeuver.cpp b/IO.SDK/Maneuvers/ApsidalAlignmentManeuver.cpp index e40b46e5..87571e81 100644 --- a/IO.SDK/Maneuvers/ApsidalAlignmentManeuver.cpp +++ b/IO.SDK/Maneuvers/ApsidalAlignmentManeuver.cpp @@ -14,16 +14,22 @@ #include -IO::SDK::Maneuvers::ApsidalAlignmentManeuver::ApsidalAlignmentManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, std::shared_ptr targetOrbit) : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator), m_targetOrbit{targetOrbit} -{ +IO::SDK::Maneuvers::ApsidalAlignmentManeuver::ApsidalAlignmentManeuver( + std::vector engines, IO::SDK::Propagators::Propagator &propagator, + std::shared_ptr targetOrbit) : IO::SDK::Maneuvers::ManeuverBase( + std::move(engines), propagator), m_targetOrbit{std::move(targetOrbit)} { } -IO::SDK::Maneuvers::ApsidalAlignmentManeuver::ApsidalAlignmentManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, std::shared_ptr targetOrbit, const IO::SDK::Time::TDB &minimumEpoch) : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator, minimumEpoch), m_targetOrbit{targetOrbit} -{ +IO::SDK::Maneuvers::ApsidalAlignmentManeuver::ApsidalAlignmentManeuver( + std::vector engines, IO::SDK::Propagators::Propagator &propagator, + std::shared_ptr targetOrbit, + const IO::SDK::Time::TDB &minimumEpoch) : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator, + minimumEpoch), + m_targetOrbit{std::move(targetOrbit)} { } -bool IO::SDK::Maneuvers::ApsidalAlignmentManeuver::CanExecute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) -{ +bool IO::SDK::Maneuvers::ApsidalAlignmentManeuver::CanExecute( + const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) { double pv = GetPTrueAnomaly(orbitalParams.GetStateVector()); double qv = GetQTrueAnomaly(orbitalParams.GetStateVector()); double v = orbitalParams.GetTrueAnomaly(); @@ -39,70 +45,66 @@ bool IO::SDK::Maneuvers::ApsidalAlignmentManeuver::CanExecute(const IO::SDK::Orb vRelativeToQ = std::fmod(vRelativeToQ, Constants::_2PI); //TODO:manage case where pv or pq == 359° and Tolerance + 2° (that does mean uppervalue ==361°) - if (vRelativeToP < Parameters::NodeDetectionAccuraccy) - { + if (vRelativeToP < Parameters::NodeDetectionAccuraccy) { m_isIntersectP = true; return true; - } - else if (vRelativeToQ < Parameters::NodeDetectionAccuraccy) - { + } else if (vRelativeToQ < Parameters::NodeDetectionAccuraccy) { m_isIntersectQ = true; return true; } return false; } -void IO::SDK::Maneuvers::ApsidalAlignmentManeuver::Compute(const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) -{ +void IO::SDK::Maneuvers::ApsidalAlignmentManeuver::Compute( + const IO::SDK::OrbitalParameters::OrbitalParameters &orbitalParams) { m_deltaV = std::make_unique(GetDeltaV(orbitalParams.GetStateVector())); m_theta = GetTheta(orbitalParams.GetStateVector()); } -IO::SDK::OrbitalParameters::StateOrientation IO::SDK::Maneuvers::ApsidalAlignmentManeuver::ComputeOrientation(const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) -{ +IO::SDK::OrbitalParameters::StateOrientation IO::SDK::Maneuvers::ApsidalAlignmentManeuver::ComputeOrientation( + const IO::SDK::OrbitalParameters::OrbitalParameters &maneuverPoint) { IO::SDK::Math::Vector3D resVector = GetDeltaV(maneuverPoint.GetStateVector()); - return IO::SDK::OrbitalParameters::StateOrientation{resVector.Normalize().To(m_spacecraft.Front), IO::SDK::Math::Vector3D(0.0, 0.0, 0.0), maneuverPoint.GetEpoch(), maneuverPoint.GetFrame()}; + return IO::SDK::OrbitalParameters::StateOrientation{resVector.Normalize().To(m_spacecraft.Front), + IO::SDK::Math::Vector3D(0.0, 0.0, 0.0), + maneuverPoint.GetEpoch(), maneuverPoint.GetFrame()}; } -bool IO::SDK::Maneuvers::ApsidalAlignmentManeuver::IsIntersectP(const IO::SDK::OrbitalParameters::StateVector &stateVector) const -{ +bool IO::SDK::Maneuvers::ApsidalAlignmentManeuver::IsIntersectP( + const IO::SDK::OrbitalParameters::StateVector &stateVector) const { double v = GetPTrueAnomaly(stateVector); auto v_vector = stateVector.GetStateVector(v).GetPosition(); - if (v_vector.GetAngle(stateVector.GetPosition()) < IO::SDK::Parameters::IntersectDetectionAccuraccy) - { + if (v_vector.GetAngle(stateVector.GetPosition()) < IO::SDK::Parameters::IntersectDetectionAccuraccy) { return true; } return false; } -bool IO::SDK::Maneuvers::ApsidalAlignmentManeuver::IsIntersectQ(const IO::SDK::OrbitalParameters::StateVector &stateVector) const -{ +bool IO::SDK::Maneuvers::ApsidalAlignmentManeuver::IsIntersectQ( + const IO::SDK::OrbitalParameters::StateVector &stateVector) const { double v = GetQTrueAnomaly(stateVector); auto v_vector = stateVector.GetStateVector(v).GetPosition(); - if (v_vector.GetAngle(stateVector.GetPosition()) < IO::SDK::Parameters::IntersectDetectionAccuraccy) - { + if (v_vector.GetAngle(stateVector.GetPosition()) < IO::SDK::Parameters::IntersectDetectionAccuraccy) { return true; } return false; } -double IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetTheta() const -{ +double IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetTheta() const { return m_theta; } -double IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetTheta(const IO::SDK::OrbitalParameters::StateVector &stateVector) const -{ +double IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetTheta( + const IO::SDK::OrbitalParameters::StateVector &stateVector) const { return stateVector.GetPerigeeVector().GetAngle(m_targetOrbit->GetPerigeeVector()); } -std::map IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetCoefficients(const IO::SDK::OrbitalParameters::StateVector &stateVector) const -{ +std::map IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetCoefficients( + const IO::SDK::OrbitalParameters::StateVector &stateVector) const { std::map res; double h1 = std::pow(stateVector.GetSpecificAngularMomentum().Magnitude(), 2.0); double h2 = std::pow(m_targetOrbit->GetSpecificAngularMomentum().Magnitude(), 2.0); @@ -116,67 +118,58 @@ std::map IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetC return res; } -double IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetPTrueAnomaly(const IO::SDK::OrbitalParameters::StateVector &sv) const -{ +double +IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetPTrueAnomaly(const IO::SDK::OrbitalParameters::StateVector &sv) const { auto coef = GetCoefficients(sv); double res = coef["alpha"] + std::acos((coef["C"] / coef["A"]) * std::cos(coef["alpha"])); - if (std::isnan(res)) - { + if (std::isnan(res)) { throw IO::SDK::Exception::InvalidArgumentException("Apsidal alignment requieres orbits intersection"); } - if (res < 0.0) - { + if (res < 0.0) { res += IO::SDK::Constants::_2PI; } return res; } -double IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetQTrueAnomaly(const IO::SDK::OrbitalParameters::StateVector &sv) const -{ +double +IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetQTrueAnomaly(const IO::SDK::OrbitalParameters::StateVector &sv) const { auto coef = GetCoefficients(sv); double res = coef["alpha"] - std::acos((coef["C"] / coef["A"]) * std::cos(coef["alpha"])); - if (std::isnan(res)) - { + if (std::isnan(res)) { throw IO::SDK::Exception::InvalidArgumentException("Apsidal alignment requieres orbits intersection"); } - if (res < 0.0) - { + if (res < 0.0) { res += IO::SDK::Constants::_2PI; } return res; } -double IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetPTargetTrueAnomaly(const IO::SDK::OrbitalParameters::StateVector &sv) const -{ +double IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetPTargetTrueAnomaly( + const IO::SDK::OrbitalParameters::StateVector &sv) const { return GetPTrueAnomaly(sv) - GetTheta(sv); } -double IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetQTargetTrueAnomaly(const IO::SDK::OrbitalParameters::StateVector &sv) const -{ +double IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetQTargetTrueAnomaly( + const IO::SDK::OrbitalParameters::StateVector &sv) const { return GetQTrueAnomaly(sv) - GetTheta(sv); } -IO::SDK::Math::Vector3D IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetDeltaV(const IO::SDK::OrbitalParameters::StateVector &sv) const -{ - if (m_deltaV) - { +IO::SDK::Math::Vector3D +IO::SDK::Maneuvers::ApsidalAlignmentManeuver::GetDeltaV(const IO::SDK::OrbitalParameters::StateVector &sv) const { + if (m_deltaV) { return *m_deltaV; } IO::SDK::Math::Vector3D resVector; - if (m_isIntersectP) - { + if (m_isIntersectP) { resVector = m_targetOrbit->GetStateVector(GetPTargetTrueAnomaly(sv)).GetVelocity() - sv.GetVelocity(); - } - else if (m_isIntersectQ) - { + } else if (m_isIntersectQ) { resVector = m_targetOrbit->GetStateVector(GetQTargetTrueAnomaly(sv)).GetVelocity() - sv.GetVelocity(); - } - else - { - throw IO::SDK::Exception::InvalidArgumentException("To compute orientation, maneuver point must be at orbits intersection"); + } else { + throw IO::SDK::Exception::InvalidArgumentException( + "To compute orientation, maneuver point must be at orbits intersection"); } return resVector; diff --git a/IO.SDK/Maneuvers/Attitudes/NadirAttitude.cpp b/IO.SDK/Maneuvers/Attitudes/NadirAttitude.cpp index deb7133c..18d8373e 100644 --- a/IO.SDK/Maneuvers/Attitudes/NadirAttitude.cpp +++ b/IO.SDK/Maneuvers/Attitudes/NadirAttitude.cpp @@ -10,13 +10,13 @@ */ #include -IO::SDK::Maneuvers::Attitudes::NadirAttitude::NadirAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, +IO::SDK::Maneuvers::Attitudes::NadirAttitude::NadirAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, attitudeHoldDuration) { } -IO::SDK::Maneuvers::Attitudes::NadirAttitude::NadirAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, +IO::SDK::Maneuvers::Attitudes::NadirAttitude::NadirAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, minimumEpoch, attitudeHoldDuration) { diff --git a/IO.SDK/Maneuvers/Attitudes/NadirAttitude.h b/IO.SDK/Maneuvers/Attitudes/NadirAttitude.h index 629e75fc..18a75684 100644 --- a/IO.SDK/Maneuvers/Attitudes/NadirAttitude.h +++ b/IO.SDK/Maneuvers/Attitudes/NadirAttitude.h @@ -51,7 +51,7 @@ namespace IO::SDK::Maneuvers::Attitudes * @param engines * @param propagator */ - NadirAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); + NadirAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); /** * @brief Construct a new Nadir Attitude object @@ -60,7 +60,7 @@ namespace IO::SDK::Maneuvers::Attitudes * @param propagator * @param minimumEpoch Not executed before this date */ - NadirAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); + NadirAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); /** * @brief Evaluate if maneuver can occurs diff --git a/IO.SDK/Maneuvers/Attitudes/ProgradeAttitude.cpp b/IO.SDK/Maneuvers/Attitudes/ProgradeAttitude.cpp index 64e0d453..9f196ff3 100644 --- a/IO.SDK/Maneuvers/Attitudes/ProgradeAttitude.cpp +++ b/IO.SDK/Maneuvers/Attitudes/ProgradeAttitude.cpp @@ -10,13 +10,13 @@ */ #include -IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::ProgradeAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, +IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::ProgradeAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, attitudeHoldDuration) { } -IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::ProgradeAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, +IO::SDK::Maneuvers::Attitudes::ProgradeAttitude::ProgradeAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, minimumEpoch, attitudeHoldDuration) { diff --git a/IO.SDK/Maneuvers/Attitudes/ProgradeAttitude.h b/IO.SDK/Maneuvers/Attitudes/ProgradeAttitude.h index 00f63cc2..0452c1c9 100644 --- a/IO.SDK/Maneuvers/Attitudes/ProgradeAttitude.h +++ b/IO.SDK/Maneuvers/Attitudes/ProgradeAttitude.h @@ -50,7 +50,7 @@ namespace IO::SDK::Maneuvers::Attitudes * @param engines * @param propagator */ - ProgradeAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); + ProgradeAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); /** * @brief Construct a new Prograde Attitude object @@ -59,7 +59,7 @@ namespace IO::SDK::Maneuvers::Attitudes * @param propagator * @param minimumEpoch */ - ProgradeAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); + ProgradeAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); /** * @brief Evaluate if maneuver can occurs diff --git a/IO.SDK/Maneuvers/Attitudes/RetrogradeAttitude.cpp b/IO.SDK/Maneuvers/Attitudes/RetrogradeAttitude.cpp index 39eb3044..e990ae48 100644 --- a/IO.SDK/Maneuvers/Attitudes/RetrogradeAttitude.cpp +++ b/IO.SDK/Maneuvers/Attitudes/RetrogradeAttitude.cpp @@ -10,11 +10,11 @@ */ #include -IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::RetrogradeAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator,attitudeHoldDuration) +IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::RetrogradeAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator,attitudeHoldDuration) { } -IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::RetrogradeAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, minimumEpoch,attitudeHoldDuration) +IO::SDK::Maneuvers::Attitudes::RetrogradeAttitude::RetrogradeAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, minimumEpoch,attitudeHoldDuration) { } diff --git a/IO.SDK/Maneuvers/Attitudes/RetrogradeAttitude.h b/IO.SDK/Maneuvers/Attitudes/RetrogradeAttitude.h index c2b2a9e1..279930f5 100644 --- a/IO.SDK/Maneuvers/Attitudes/RetrogradeAttitude.h +++ b/IO.SDK/Maneuvers/Attitudes/RetrogradeAttitude.h @@ -50,7 +50,7 @@ namespace IO::SDK::Maneuvers::Attitudes * @param engines * @param propagator */ - RetrogradeAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); + RetrogradeAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); /** * @brief Construct a new Retrograde Attitude object @@ -59,7 +59,7 @@ namespace IO::SDK::Maneuvers::Attitudes * @param propagator * @param minimumEpoch */ - RetrogradeAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); + RetrogradeAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration); /** * @brief Evaluate if maneuver can occurs diff --git a/IO.SDK/Maneuvers/Attitudes/TowardObjectAttitude.cpp b/IO.SDK/Maneuvers/Attitudes/TowardObjectAttitude.cpp index 674b24e3..77584c07 100644 --- a/IO.SDK/Maneuvers/Attitudes/TowardObjectAttitude.cpp +++ b/IO.SDK/Maneuvers/Attitudes/TowardObjectAttitude.cpp @@ -10,7 +10,7 @@ */ #include -IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::TowardObjectAttitude(const std::vector engines, +IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::TowardObjectAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, attitudeHoldDuration), @@ -18,7 +18,7 @@ IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::TowardObjectAttitude(const { } -IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::TowardObjectAttitude(const std::vector engines, +IO::SDK::Maneuvers::Attitudes::TowardObjectAttitude::TowardObjectAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration, const IO::SDK::Body::Body &targetBody) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, minimumEpoch, attitudeHoldDuration), m_targetBody{targetBody} diff --git a/IO.SDK/Maneuvers/Attitudes/TowardObjectAttitude.h b/IO.SDK/Maneuvers/Attitudes/TowardObjectAttitude.h index c75f540e..aa68bb71 100644 --- a/IO.SDK/Maneuvers/Attitudes/TowardObjectAttitude.h +++ b/IO.SDK/Maneuvers/Attitudes/TowardObjectAttitude.h @@ -51,7 +51,7 @@ namespace IO::SDK::Maneuvers::Attitudes * @param propagator * @param targetBody */ - TowardObjectAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration, const IO::SDK::Body::Body &targetBody); + TowardObjectAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator,const IO::SDK::Time::TimeSpan& attitudeHoldDuration, const IO::SDK::Body::Body &targetBody); /** * @brief Construct a new Toward Object Attitude object @@ -61,7 +61,7 @@ namespace IO::SDK::Maneuvers::Attitudes * @param minimumEpoch * @param targetBody */ - TowardObjectAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration, const IO::SDK::Body::Body &targetBody); + TowardObjectAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch,const IO::SDK::Time::TimeSpan& attitudeHoldDuration, const IO::SDK::Body::Body &targetBody); /** * @brief Evaluate if maneuver can occurs diff --git a/IO.SDK/Maneuvers/Attitudes/ZenithAttitude.cpp b/IO.SDK/Maneuvers/Attitudes/ZenithAttitude.cpp index 8de3ffac..f9e9a1a4 100644 --- a/IO.SDK/Maneuvers/Attitudes/ZenithAttitude.cpp +++ b/IO.SDK/Maneuvers/Attitudes/ZenithAttitude.cpp @@ -10,12 +10,12 @@ */ #include -IO::SDK::Maneuvers::Attitudes::ZenithAttitude::ZenithAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, +IO::SDK::Maneuvers::Attitudes::ZenithAttitude::ZenithAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, attitudeHoldDuration) { } -IO::SDK::Maneuvers::Attitudes::ZenithAttitude::ZenithAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, +IO::SDK::Maneuvers::Attitudes::ZenithAttitude::ZenithAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, minimumEpoch, attitudeHoldDuration) { } diff --git a/IO.SDK/Maneuvers/Attitudes/ZenithAttitude.h b/IO.SDK/Maneuvers/Attitudes/ZenithAttitude.h index c789aebf..f2c4bfe9 100644 --- a/IO.SDK/Maneuvers/Attitudes/ZenithAttitude.h +++ b/IO.SDK/Maneuvers/Attitudes/ZenithAttitude.h @@ -50,7 +50,7 @@ namespace IO::SDK::Maneuvers::Attitudes * @param engines * @param propagator */ - ZenithAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration); + ZenithAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TimeSpan &attitudeHoldDuration); /** * @brief Construct a new Zenith Attitude object @@ -59,7 +59,7 @@ namespace IO::SDK::Maneuvers::Attitudes * @param propagator * @param minimumEpoch */ - ZenithAttitude(const std::vector engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration); + ZenithAttitude(const std::vector& engines, IO::SDK::Propagators::Propagator &propagator, const IO::SDK::Time::TDB &minimumEpoch, const IO::SDK::Time::TimeSpan &attitudeHoldDuration); /** * @brief Evaluate if maneuver can occurs diff --git a/IO.SDK/Maneuvers/CombinedManeuver.cpp b/IO.SDK/Maneuvers/CombinedManeuver.cpp index cfcb245e..143c3972 100644 --- a/IO.SDK/Maneuvers/CombinedManeuver.cpp +++ b/IO.SDK/Maneuvers/CombinedManeuver.cpp @@ -13,11 +13,13 @@ #include #include -IO::SDK::Maneuvers::CombinedManeuver::CombinedManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, const double inclination, const double perigeeRadius) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator), m_inclination{inclination}, m_peregeeRadius{perigeeRadius} +#include + +IO::SDK::Maneuvers::CombinedManeuver::CombinedManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, const double inclination, const double perigeeRadius) : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator), m_inclination{inclination}, m_peregeeRadius{perigeeRadius} { } -IO::SDK::Maneuvers::CombinedManeuver::CombinedManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, const double inclination, const double perigeeRadius, const IO::SDK::Time::TDB &minimumEpoch) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, minimumEpoch), m_inclination{inclination}, m_peregeeRadius{perigeeRadius} +IO::SDK::Maneuvers::CombinedManeuver::CombinedManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, const double inclination, const double perigeeRadius, const IO::SDK::Time::TDB &minimumEpoch) : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator, minimumEpoch), m_inclination{inclination}, m_peregeeRadius{perigeeRadius} { } diff --git a/IO.SDK/Maneuvers/CombinedManeuver.h b/IO.SDK/Maneuvers/CombinedManeuver.h index 32387a28..9b4a1321 100644 --- a/IO.SDK/Maneuvers/CombinedManeuver.h +++ b/IO.SDK/Maneuvers/CombinedManeuver.h @@ -30,7 +30,6 @@ namespace IO::SDK::Maneuvers class CombinedManeuver final : public IO::SDK::Maneuvers::ManeuverBase { private: - double m_relativeInclination{}; double m_inclination; double m_peregeeRadius; diff --git a/IO.SDK/Maneuvers/Launch.h b/IO.SDK/Maneuvers/Launch.h index 69247e51..8d89e0e0 100644 --- a/IO.SDK/Maneuvers/Launch.h +++ b/IO.SDK/Maneuvers/Launch.h @@ -42,7 +42,6 @@ namespace IO::SDK::Maneuvers double m_inertialDescendingAzimuthLaunch{std::numeric_limits::quiet_NaN()}; double m_nonInertialDescendingAzimuthLaunch{std::numeric_limits::quiet_NaN()}; double m_nonInertialInsertionVelocity{std::numeric_limits::quiet_NaN()}; - double m_inertialInsertionVelocity{std::numeric_limits::quiet_NaN()}; const double m_deltaL{std::numeric_limits::quiet_NaN()}; const double m_inclination{std::numeric_limits::quiet_NaN()}; diff --git a/IO.SDK/Maneuvers/OrbitalPlaneChangingManeuver.cpp b/IO.SDK/Maneuvers/OrbitalPlaneChangingManeuver.cpp index 21771049..14663263 100644 --- a/IO.SDK/Maneuvers/OrbitalPlaneChangingManeuver.cpp +++ b/IO.SDK/Maneuvers/OrbitalPlaneChangingManeuver.cpp @@ -17,14 +17,14 @@ IO::SDK::Maneuvers::OrbitalPlaneChangingManeuver::OrbitalPlaneChangingManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, std::shared_ptr targetOrbit) : IO::SDK::Maneuvers::ManeuverBase( - std::move(engines), propagator), m_targetOrbit{targetOrbit} + std::move(engines), propagator), m_targetOrbit{std::move(targetOrbit)} { } IO::SDK::Maneuvers::OrbitalPlaneChangingManeuver::OrbitalPlaneChangingManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, std::shared_ptr targetOrbit, const IO::SDK::Time::TDB &minimumEpoch) - : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator, minimumEpoch), m_targetOrbit{targetOrbit} + : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator, minimumEpoch), m_targetOrbit{std::move(targetOrbit)} { } diff --git a/IO.SDK/Maneuvers/PerigeeHeightChangingManeuver.cpp b/IO.SDK/Maneuvers/PerigeeHeightChangingManeuver.cpp index 18d83807..fa5e5dbe 100644 --- a/IO.SDK/Maneuvers/PerigeeHeightChangingManeuver.cpp +++ b/IO.SDK/Maneuvers/PerigeeHeightChangingManeuver.cpp @@ -12,15 +12,17 @@ #include #include +#include + IO::SDK::Maneuvers::PerigeeHeightChangingManeuver::PerigeeHeightChangingManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, double targetHeight) - : IO::SDK::Maneuvers::ManeuverBase(engines, propagator), m_targetHeight{targetHeight} + : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator), m_targetHeight{targetHeight} { } IO::SDK::Maneuvers::PerigeeHeightChangingManeuver::PerigeeHeightChangingManeuver(std::vector engines, IO::SDK::Propagators::Propagator &propagator, double targetHeight, - const IO::SDK::Time::TDB &minimumEpoch) : IO::SDK::Maneuvers::ManeuverBase(engines, propagator, + const IO::SDK::Time::TDB &minimumEpoch) : IO::SDK::Maneuvers::ManeuverBase(std::move(engines), propagator, minimumEpoch), m_targetHeight{targetHeight} { diff --git a/IO.SDK/OrbitalParameters/OrbitalParameters.cpp b/IO.SDK/OrbitalParameters/OrbitalParameters.cpp index 374a8478..576c3144 100644 --- a/IO.SDK/OrbitalParameters/OrbitalParameters.cpp +++ b/IO.SDK/OrbitalParameters/OrbitalParameters.cpp @@ -13,7 +13,9 @@ #include #include -IO::SDK::OrbitalParameters::OrbitalParameters::OrbitalParameters(const std::shared_ptr ¢erOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame) : m_centerOfMotion{centerOfMotion}, m_epoch{epoch}, m_frame{frame} +#include + +IO::SDK::OrbitalParameters::OrbitalParameters::OrbitalParameters(const std::shared_ptr ¢erOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame) : m_centerOfMotion{centerOfMotion}, m_epoch{std::move(epoch)}, m_frame{std::move(frame)} { } diff --git a/IO.SDK/OrbitalParameters/OrbitalParameters.h b/IO.SDK/OrbitalParameters/OrbitalParameters.h index 0e102a3d..326f2aca 100644 --- a/IO.SDK/OrbitalParameters/OrbitalParameters.h +++ b/IO.SDK/OrbitalParameters/OrbitalParameters.h @@ -46,7 +46,7 @@ namespace IO::SDK::OrbitalParameters * @param epoch * @param frame */ - OrbitalParameters(const std::shared_ptr ¢erOfMotion, const IO::SDK::Time::TDB &epoch, const IO::SDK::Frames::Frames &frame); + OrbitalParameters(const std::shared_ptr ¢erOfMotion, IO::SDK::Time::TDB epoch, IO::SDK::Frames::Frames frame); virtual ~OrbitalParameters() = default; diff --git a/IO.SDK/Propagators/Propagator.cpp b/IO.SDK/Propagators/Propagator.cpp index e81458b6..f78f0b72 100644 --- a/IO.SDK/Propagators/Propagator.cpp +++ b/IO.SDK/Propagators/Propagator.cpp @@ -10,7 +10,6 @@ */ #include #include -#include #include #include diff --git a/IO.SDK/Scenario/Scenario.h b/IO.SDK/Scenario/Scenario.h index f5ee48c1..89791909 100644 --- a/IO.SDK/Scenario/Scenario.h +++ b/IO.SDK/Scenario/Scenario.h @@ -113,52 +113,8 @@ namespace IO::SDK inline Propagators::Propagator &GetPropagator() { return *m_propagator; } - - - /** - * Add a distance constraint - * @param distanceParameters - */ - void AddDistanceConstraint(Constraints::Parameters::DistanceParameters *distanceParameters); - - /** - * Add an occultation constraint - * @param occultationParameters - */ - void AddOccultationConstraint(IO::SDK::Constraints::Parameters::OccultationParameters *occultationParameters); - - /** - * Add a day constraint - * @param byDayParameters - */ - void AddDayConstraint(IO::SDK::Constraints::Parameters::ByDayParameters *byDayParameters); - - /** - * Add a night constraint - * @param byNightParameters - */ - void AddNightConstraint(IO::SDK::Constraints::Parameters::ByNightParameters *byNightParameters); - - /** - * Add a body visibility constraint - * @param bodyVisibilityParameters - */ - void AddBodyVisibilityConstraint(IO::SDK::Constraints::Parameters::BodyVisibilityFromSiteParameters *bodyVisibilityParameters); - - /** - * Add a field of view constraint - * @param inFieldOfViewParameters - */ - void AddInFieldOfViewConstraint(IO::SDK::Constraints::Parameters::InFieldOfViewParameters *inFieldOfViewParameters); - - /** - * Add launch constraint - * @param launchParameters - */ - void AddLaunchConstraint(IO::SDK::Constraints::Parameters::LaunchParameters *launchParameters); - /** - * Execute scenario, propagate spacecrafts, simulate maneuvers, evaluate constraints + * Execute scenario */ void Execute(); }; diff --git a/IO.SDK/Sites/LaunchSite.cpp b/IO.SDK/Sites/LaunchSite.cpp index 03e39482..81366bae 100644 --- a/IO.SDK/Sites/LaunchSite.cpp +++ b/IO.SDK/Sites/LaunchSite.cpp @@ -15,7 +15,7 @@ #include IO::SDK::Sites::LaunchSite::LaunchSite(const int id, const std::string &name, const IO::SDK::Coordinates::Geodetic &coordinates, - std::shared_ptr body, std::string directoryPath) : Site(id, name, coordinates, body, std::move(directoryPath)) + std::shared_ptr body, std::string directoryPath) : Site(id, name, coordinates, std::move(body), std::move(directoryPath)) { }