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(); } }
//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; } }