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Path: SpacecraftEstimation/Demos/OrbitEstimation
% Test the orbit Kalman Filter with omni and GPS measurements. The simulation and the filter both use the same RHS, FOrbKF, but the simulation uses more terms in the gravity model. ------------------------------------------------------------------------ See also CDKF45, OrbitKFRHS, HRangeMeasurement, RangeMeasurement, GPSReceiver, and FOrbKF, Plot2D, TimeGUI, Cross, RK4, RK45, Date2JD, JD2T, LoadGravityModel, OrbRate, El2RV, Period, EarthRot, EarthRte, GPSSatellite, Omni ------------------------------------------------------------------------ % ------------------------------------------------------------------------------- Copyright (c) 2001-2003 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------------
AC: ACData/ACTConstants AerospaceUtils: Coord/IntersectPlanet Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: GUIs/TimeGUI Common: General/CellToMat Common: General/CloseIfHandle Common: General/DeBlankLT Common: General/DeleteCell Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Ellipsd Common: Graphics/Map Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Common: Time/T2JD Math: Analysis/Jacobian Math: Integration/RK4 Math: Integration/RK45 Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Factorl Math: Linear/Mag Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD Orbit: GravityModels/LoadGEM Orbit: GravityModels/LoadGravityModel Orbit: GravityModels/NormalizationMatrix Orbit: GravityModels/UnnormalizeGravity Orbit: OrbitMechanics/AGravityC Orbit: OrbitMechanics/APlanet Orbit: OrbitMechanics/PlanetaryAccelerations SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/El2RV SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/OrbRate SC: BasicOrbit/Period SC: BasicOrbit/RV2A SC: BasicOrbit/RV2El SC: BasicOrbit/RVFromKepler SC: Ephem/ECIToPlanet SC: Ephem/EOfE SC: Ephem/EarthNut SC: Ephem/EarthPre SC: Ephem/EarthRot SC: Ephem/EarthRte SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/MoonRot SC: Ephem/MoonV1 SC: Ephem/Moons SC: Ephem/NutDelta SC: Ephem/ObOfE SC: Ephem/SunV1 SC: Ephem/TruEarth SC: SCData/sCTConstants SC: SCMat/GEMT1 SCPro: ProSensors/GPSReceiver SCPro: ProSensors/GPSSatellite SCPro: ProSensors/RangeMeasurement SpacecraftEstimation: OrbitEstimation/CDKF45 SpacecraftEstimation: OrbitEstimation/FOrbKF SpacecraftEstimation: OrbitEstimation/HRangeMeasurement SpacecraftEstimation: OrbitEstimation/OrbitKFRHS SpacecraftEstimation: OrbitEstimation/ReshapeCovariance
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