Features/uprage native library (#96)

* Remove propagator into native library

* minor fixes

* Upgrade native libraries

IO.Astrodynamics.CLI/IO.Astrodynamics.CLI.csproj

@@ -9,7 +9,7 @@
         <FileVersion>0.0.1</FileVersion>
         <PackAsTool>true</PackAsTool>
         <ToolCommandName>astro</ToolCommandName>
-        <Version>0.1.6</Version>
+        <Version>0.1.7</Version>
         <Title>Astrodynamics command line interface</Title>
         <Authors>Sylvain Guillet</Authors>
         <Description>This CLI allows end user to exploit IO.Astrodynamics framework </Description>

IO.Astrodynamics.Performance/Scenario.cs

@@ -19,7 +19,7 @@ namespace IO.Astrodynamics.Performance;
 [SkewnessColumn]
 [KurtosisColumn]
 [StatisticalTestColumn]
-// [ShortRunJob]
+[ShortRunJob]
 public class Scenario
 {
     private readonly GeopotentialGravitationalField _geopotential;
@@ -43,18 +43,18 @@ public Scenario()
         Spacecraft spc = new Spacecraft(-1001, "MySpacecraft", 100.0, 10000.0, clk,
             new StateVector(new Vector3(6800000.0, 0.0, 0.0), new Vector3(0.0, 7656.2204182967143, 0.0), _earth, DateTimeExtension.J2000, Frames.Frame.ICRF));
         _srp = new SolarRadiationPressure(spc);
-        _atm = new AtmosphericDrag(spc,_earth);
+        _atm = new AtmosphericDrag(spc, _earth);
         List<ForceBase> forces = new List<ForceBase>();
         forces.Add(new GravitationalAcceleration(_sun));
         forces.Add(new GravitationalAcceleration(_moon));
         forces.Add(new GravitationalAcceleration(_earth));
-        forces.Add(new AtmosphericDrag(spc,_earth));
+        forces.Add(new AtmosphericDrag(spc, _earth));
         forces.Add(new SolarRadiationPressure(spc));
         _integrator = new VVIntegrator(forces, TimeSpan.FromSeconds(1.0), new StateVector(new Vector3(6800000.0 - Random.Shared.NextDouble(), 0.0, 0.0),
             new Vector3(0.0, 8000.0 - Random.Shared.NextDouble(), 0.0), _earth,
             DateTimeExtension.J2000, Frame.ICRF));
         _spacecraftPropagator = new Propagator.SpacecraftPropagator(new Window(DateTimeExtension.J2000, DateTimeExtension.J2000 + spc.InitialOrbitalParameters.Period()), spc,
-            new[] { _moon }, true, true, TimeSpan.FromSeconds(1.0));
+            new[] { _moon, _earth, _sun }, true, true, TimeSpan.FromSeconds(1.0));
     }
 
     // [Benchmark(Description = "Spacecraft spacecraftPropagator C++")]

IO.Astrodynamics/API.cs

@@ -592,17 +592,16 @@ public IEnumerable<LaunchWindow> FindLaunchWindows(Maneuver.Launch launch,
         ILocalizable observer, ILocalizable target, Frame frame,
         Aberration aberration, TimeSpan stepSize)
     {
-        if (observer == null) throw new ArgumentNullException(nameof(observer));
-        if (target == null) throw new ArgumentNullException(nameof(target));
-        if (frame == null) throw new ArgumentNullException(nameof(frame));
+        ArgumentNullException.ThrowIfNull(observer);
+        ArgumentNullException.ThrowIfNull(target);
+        ArgumentNullException.ThrowIfNull(frame);
         lock (lockObject)
         {
             const int messageSize = 10000;
             List<OrbitalParameters.OrbitalParameters> orbitalParameters = [];
-            int occurences = (int)(searchWindow.Length / stepSize / messageSize);
-
+            int occurrences = (int)(searchWindow.Length / stepSize / messageSize);
 
-            for (int i = 0; i <= occurences; i++)
+            for (int i = 0; i <= occurrences; i++)
             {
                 var start = searchWindow.StartDate + i * messageSize * stepSize;
                 var end = start + messageSize * stepSize > searchWindow.EndDate ? searchWindow.EndDate : (start + messageSize * stepSize) - stepSize;
@@ -632,9 +631,9 @@ public IEnumerable<LaunchWindow> FindLaunchWindows(Maneuver.Launch launch,
     public OrbitalParameters.OrbitalParameters ReadEphemeris(DateTime epoch, ILocalizable observer,
         ILocalizable target, Frame frame, Aberration aberration)
     {
-        if (observer == null) throw new ArgumentNullException(nameof(observer));
-        if (target == null) throw new ArgumentNullException(nameof(target));
-        if (frame == null) throw new ArgumentNullException(nameof(frame));
+        ArgumentNullException.ThrowIfNull(observer);
+        ArgumentNullException.ThrowIfNull(target);
+        ArgumentNullException.ThrowIfNull(frame);
         lock (lockObject)
         {
             if (frame == null) throw new ArgumentNullException(nameof(frame));
@@ -731,7 +730,7 @@ public CelestialBody GetCelestialBodyInfo(int naifId)
     {
         lock (lockObject)
         {
-           return GetCelestialBodyInfoProxy(naifId);
+            return GetCelestialBodyInfoProxy(naifId);
         }
     }
 

IO.Astrodynamics/IO.Astrodynamics.csproj

@@ -43,14 +43,14 @@
 
     <ItemGroup>
       <None Remove="resources\IO.Astrodynamics.dll" />
+      <None Remove="resources\IO.Astrodynamics.lib" />
+      <None Remove="resources\libIO.Astrodynamics.so" />
       <Content Include="resources\IO.Astrodynamics.dll">
         <CopyToOutputDirectory>Always</CopyToOutputDirectory>
       </Content>
-      <None Remove="resources\IO.Astrodynamics.lib" />
       <Content Include="resources\IO.Astrodynamics.lib">
         <CopyToOutputDirectory>Always</CopyToOutputDirectory>
       </Content>
-      <None Remove="resources\libIO.Astrodynamics.so" />
       <Content Include="resources\libIO.Astrodynamics.so">
         <CopyToOutputDirectory>Always</CopyToOutputDirectory>
       </Content>

IO.Astrodynamics/IO.Astrodynamics.nuspec

@@ -4,7 +4,7 @@
         <id>IO.Astrodynamics</id>
         <authors>Sylvain Guillet</authors>
         <copyright>Sylvain Guillet</copyright>
-        <version>3.0.2</version>
+        <version>3.0.3</version>
         <title>Astrodynamics framework</title>
         <icon>images\dragonfly-dark-trans.png</icon>
         <readme>docs\README.md</readme>