public void set_InitStateJx(object InitStateObj, string name, double value)
{
if (name == "SemiMajorAxis")
{
SemiMajorAxis = value;
}
else if (name == "Eccentricity")
{
Eccentricity = value;
}
else if (name == "Inclination")
{
Inclination = value;
}
else if (name == "ArgOfPerigee")
{
ArgOfPerigee = value;
}
else if (name == "RAAN")
{
RAAN = value;
}
else if (name == "TrueAnomaly")
{
TrueAnomaly = value;
}
IAgSatellite sat = InitStateObj as IAgSatellite;
if (sat.PropagatorType == AgEVePropagatorType.ePropagatorJ2Perturbation)
{
IAgVePropagatorJ2Perturbation prop = sat.Propagator as IAgVePropagatorJ2Perturbation;
prop.InitialState.Representation.AssignClassical(AgECoordinateSystem.eCoordinateSystemICRF, SemiMajorAxis, Eccentricity, Inclination, ArgOfPerigee, RAAN, TrueAnomaly);
prop.Propagate();
}
if (sat.PropagatorType == AgEVePropagatorType.ePropagatorJ4Perturbation)
{
IAgVePropagatorJ4Perturbation prop = sat.Propagator as IAgVePropagatorJ4Perturbation;
prop.InitialState.Representation.AssignClassical(AgECoordinateSystem.eCoordinateSystemICRF, SemiMajorAxis, Eccentricity, Inclination, ArgOfPerigee, RAAN, TrueAnomaly);
prop.Propagate();
}
if (sat.PropagatorType == AgEVePropagatorType.ePropagatorTwoBody)
{
IAgVePropagatorTwoBody prop = sat.Propagator as IAgVePropagatorTwoBody;
prop.InitialState.Representation.AssignClassical(AgECoordinateSystem.eCoordinateSystemICRF, SemiMajorAxis, Eccentricity, Inclination, ArgOfPerigee, RAAN, TrueAnomaly);
prop.Propagate();
}
}
public Satellite_OrbitData(IAgStkObject Object0)
{
m_ElemsType = "Classical";
if (Object0.ClassName == "Satellite")
{
IAgSatellite sat = Object0 as IAgSatellite;
if (sat.PropagatorType == AgEVePropagatorType.ePropagatorJ2Perturbation)
{
IAgVePropagatorJ2Perturbation prop = sat.Propagator as IAgVePropagatorJ2Perturbation;
m_ObjectTimes = prop.EphemerisInterval as AgCrdnEventIntervalSmartInterval;
Step_Size = prop.Step;
IAgOrbitStateClassical keplerState = prop.InitialState.Representation.ConvertTo(AgEOrbitStateType.eOrbitStateClassical) as IAgOrbitStateClassical;
m_ultimateObject = Object0;
get_InitStateJx(keplerState);
}
else if (sat.PropagatorType == AgEVePropagatorType.ePropagatorJ4Perturbation)
{
IAgVePropagatorJ4Perturbation prop = sat.Propagator as IAgVePropagatorJ4Perturbation;
m_ObjectTimes = prop.EphemerisInterval as AgCrdnEventIntervalSmartInterval;
Step_Size = prop.Step;
IAgOrbitStateClassical keplerState = prop.InitialState.Representation.ConvertTo(AgEOrbitStateType.eOrbitStateClassical) as IAgOrbitStateClassical;
m_ultimateObject = keplerState;
get_InitStateJx(keplerState);
}
else if (sat.PropagatorType == AgEVePropagatorType.ePropagatorTwoBody)
{
IAgVePropagatorTwoBody prop = sat.Propagator as IAgVePropagatorTwoBody;
m_ObjectTimes = prop.EphemerisInterval as AgCrdnEventIntervalSmartInterval;
Step_Size = prop.Step;
IAgOrbitStateClassical keplerState = prop.InitialState.Representation.ConvertTo(AgEOrbitStateType.eOrbitStateClassical) as IAgOrbitStateClassical;
m_ultimateObject = keplerState;
get_InitStateJx(keplerState);
}
}
}
//Satellite helpers
public static void ChangeSatelliteInterval(IAgSatellite sat, string startTime, string stopTime, bool astgRun)
{
AgEVePropagatorType propType = sat.PropagatorType;
//IAgVePropagator prop = sat.Propagator;
switch (propType)
{
case AgEVePropagatorType.eUnknownPropagator:
break;
case AgEVePropagatorType.ePropagatorHPOP:
IAgVePropagatorHPOP prop = sat.Propagator as IAgVePropagatorHPOP;
prop.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
prop.Propagate();
break;
case AgEVePropagatorType.ePropagatorJ2Perturbation:
IAgVePropagatorJ2Perturbation prop1 = sat.Propagator as IAgVePropagatorJ2Perturbation;
prop1.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
prop1.Propagate();
break;
case AgEVePropagatorType.ePropagatorJ4Perturbation:
IAgVePropagatorJ4Perturbation prop2 = sat.Propagator as IAgVePropagatorJ4Perturbation;
prop2.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
prop2.Propagate();
break;
case AgEVePropagatorType.ePropagatorLOP:
IAgVePropagatorLOP prop3 = sat.Propagator as IAgVePropagatorLOP;
prop3.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
prop3.Propagate();
break;
case AgEVePropagatorType.ePropagatorSGP4:
IAgVePropagatorSGP4 prop4 = sat.Propagator as IAgVePropagatorSGP4;
prop4.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
prop4.Propagate();
break;
case AgEVePropagatorType.ePropagatorSPICE:
IAgVePropagatorSPICE prop5 = sat.Propagator as IAgVePropagatorSPICE;
prop5.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
prop5.Propagate();
break;
case AgEVePropagatorType.ePropagatorStkExternal:
IAgVePropagatorStkExternal prop6 = sat.Propagator as IAgVePropagatorStkExternal;
//prop6.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
break;
case AgEVePropagatorType.ePropagatorTwoBody:
IAgVePropagatorTwoBody prop7 = sat.Propagator as IAgVePropagatorTwoBody;
prop7.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
prop7.Propagate();
break;
case AgEVePropagatorType.ePropagatorUserExternal:
break;
case AgEVePropagatorType.ePropagatorGreatArc:
IAgVePropagatorGreatArc prop8 = sat.Propagator as IAgVePropagatorGreatArc;
prop8.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
prop8.Propagate();
break;
case AgEVePropagatorType.ePropagatorBallistic:
break;
case AgEVePropagatorType.ePropagatorSimpleAscent:
break;
case AgEVePropagatorType.ePropagatorAstrogator:
if (astgRun)
{
IAgVADriverMCS driver = sat.Propagator as IAgVADriverMCS;
driver.RunMCS();
}
break;
case AgEVePropagatorType.ePropagatorRealtime:
break;
case AgEVePropagatorType.ePropagatorGPS:
IAgVePropagatorGPS prop9 = sat.Propagator as IAgVePropagatorGPS;
prop9.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
prop9.Propagate();
break;
case AgEVePropagatorType.ePropagatorAviator:
break;
case AgEVePropagatorType.ePropagator11Param:
IAgVePropagator11Param prop10 = sat.Propagator as IAgVePropagator11Param;
prop10.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
prop10.Propagate();
break;
case AgEVePropagatorType.ePropagatorSP3:
IAgVePropagatorSP3 prop11 = sat.Propagator as IAgVePropagatorSP3;
//prop11.EphemerisInterval.SetExplicitInterval(startTime, stopTime);
break;
default:
break;
}
}