From f30341511f9c4ffc4d69afa52cc644a2395bfb2d Mon Sep 17 00:00:00 2001 From: Alder Date: Wed, 6 Mar 2024 23:30:36 +0100 Subject: [PATCH] update alicia and im schema --- .../schema/v3_4_alicia/cpacs_schema.xsd | 453 +++++++++++++++--- .../v3_4_impactMonitor/cpacs_schema.xsd | 453 +++++++++++++++--- 2 files changed, 770 insertions(+), 136 deletions(-) diff --git a/addContent/schema/v3_4_alicia/cpacs_schema.xsd b/addContent/schema/v3_4_alicia/cpacs_schema.xsd index f6b80804..1bd62fa7 100644 --- a/addContent/schema/v3_4_alicia/cpacs_schema.xsd +++ b/addContent/schema/v3_4_alicia/cpacs_schema.xsd @@ -2986,6 +2986,7 @@ cpacs@dlr.de + @@ -3644,6 +3645,35 @@ cpacs@dlr.de + + + + + + Approach procedures + + + + + + + + + + + RNP approach + + + + + RNAV approach + + + + + + + @@ -14313,52 +14343,6 @@ cpacs@dlr.de - - - - - - Participants - - - - - - - - - - - - - - - - - - - - - - Participant - - - - - - - - - - - - - - - - - - @@ -17510,6 +17494,35 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + + ILS approach + + + + + + + + + + Name + + + + + UID of the ILS defined for the airport runway + + + + + + + + @@ -22479,6 +22492,13 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + UID of the approach procedure + + + @@ -25535,6 +25555,52 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + + Participants + + + + + + + + + + + + + + + + + + + + + + Participant + + + + + + + + + + + + + + + + + + @@ -26602,6 +26668,43 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + + Point: x,y,z + + + Point type, containing an obligatory xyz data triplet. + + + + + + + + + + X-Component + + + + + Y-Component + + + + + Z-Component + + + + + + + + @@ -28649,6 +28752,216 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + + Curve + + + + + + + + + + Turn angle + + + + + Path angle + + + + + Radius + + + + + + + + + + + + + + + + + + + + + Direct + + + + + + + + + + Path angle + + + + + Path length + + + + + + + + + + + + + Constraints + + + + + + + + + + + + + + + + + + + + Segments + + + + + + + + + + + + + + + + + + + + Segment + + + + + + + + + + + + + + + + + + + + End condition + + + + + + + + + + + + + + Start/end condition + + + + + + + + + + + Global coordinate at the start in xyz coordinates + + + + + Global coordinate at the start in geographic coordinates (longitude, latitude, altitude) + + + + + + + + + + + + + + + + RNP/RNAV approach + + + + + + + + + + Name + + + + + UID of the runway + + + + + Start condition + + + + + + + + + @@ -29633,12 +29946,8 @@ The fuel tank volume type should also be used for the wing fuel tank - runwayILSType + Runway ILS - - RunwayILS type, containing ILS data of a runway - - @@ -29651,20 +29960,19 @@ The fuel tank volume type should also be used for the wing fuel tank - - - - Position of the glide slope antenna - - - - - - Angle of the glide path - - - + + + Position of the glide slope antenna + + + + + + Angle of the glide path + + + @@ -29802,22 +30110,22 @@ The fuel tank volume type should also be used for the wing fuel tankRunway heading - + Takeoff run available - + Landing distance available - + Conditions of the runway - + @@ -34436,6 +34744,15 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + Waypoint + + + + diff --git a/addContent/schema/v3_4_impactMonitor/cpacs_schema.xsd b/addContent/schema/v3_4_impactMonitor/cpacs_schema.xsd index f6b80804..1bd62fa7 100644 --- a/addContent/schema/v3_4_impactMonitor/cpacs_schema.xsd +++ b/addContent/schema/v3_4_impactMonitor/cpacs_schema.xsd @@ -2986,6 +2986,7 @@ cpacs@dlr.de + @@ -3644,6 +3645,35 @@ cpacs@dlr.de + + + + + + Approach procedures + + + + + + + + + + + RNP approach + + + + + RNAV approach + + + + + + + @@ -14313,52 +14343,6 @@ cpacs@dlr.de - - - - - - Participants - - - - - - - - - - - - - - - - - - - - - - Participant - - - - - - - - - - - - - - - - - - @@ -17510,6 +17494,35 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + + ILS approach + + + + + + + + + + Name + + + + + UID of the ILS defined for the airport runway + + + + + + + + @@ -22479,6 +22492,13 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + UID of the approach procedure + + + @@ -25535,6 +25555,52 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + + Participants + + + + + + + + + + + + + + + + + + + + + + Participant + + + + + + + + + + + + + + + + + + @@ -26602,6 +26668,43 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + + Point: x,y,z + + + Point type, containing an obligatory xyz data triplet. + + + + + + + + + + X-Component + + + + + Y-Component + + + + + Z-Component + + + + + + + + @@ -28649,6 +28752,216 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + + Curve + + + + + + + + + + Turn angle + + + + + Path angle + + + + + Radius + + + + + + + + + + + + + + + + + + + + + Direct + + + + + + + + + + Path angle + + + + + Path length + + + + + + + + + + + + + Constraints + + + + + + + + + + + + + + + + + + + + Segments + + + + + + + + + + + + + + + + + + + + Segment + + + + + + + + + + + + + + + + + + + + End condition + + + + + + + + + + + + + + Start/end condition + + + + + + + + + + + Global coordinate at the start in xyz coordinates + + + + + Global coordinate at the start in geographic coordinates (longitude, latitude, altitude) + + + + + + + + + + + + + + + + RNP/RNAV approach + + + + + + + + + + Name + + + + + UID of the runway + + + + + Start condition + + + + + + + + + @@ -29633,12 +29946,8 @@ The fuel tank volume type should also be used for the wing fuel tank - runwayILSType + Runway ILS - - RunwayILS type, containing ILS data of a runway - - @@ -29651,20 +29960,19 @@ The fuel tank volume type should also be used for the wing fuel tank - - - - Position of the glide slope antenna - - - - - - Angle of the glide path - - - + + + Position of the glide slope antenna + + + + + + Angle of the glide path + + + @@ -29802,22 +30110,22 @@ The fuel tank volume type should also be used for the wing fuel tankRunway heading - + Takeoff run available - + Landing distance available - + Conditions of the runway - + @@ -34436,6 +34744,15 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + Waypoint + + + +