Path: SpacecraftEstimation/UKF
% UKF orbit angles Tracks a spacecraft using orbit angles from a ground station. Things to try; 1. Add more ground stations 2. Try different orbits 3. Try different covariances and initial estimator states ------------------------------------------------------------------------- % ------------------------------------------------------------------------- Copyright (c) 2015 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------
AC: ACData/ACTConstants AerospaceUtils: Coord/LatLonAltToEF SC: BasicOrbit/CP2I 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/Period SC: Ephem/EOfE SC: Ephem/EarthRot SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/NutDelta SC: Ephem/ObOfE SC: SCData/sCTConstants SpacecraftEstimation: DemoFuns/LatLonToNEU SpacecraftEstimation: DemoFuns/RHSEarthOrbitUKF SpacecraftEstimation: DemoFuns/TelescopeUKF Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: Estimation/KFInitialize Common: Estimation/UKFPredict Common: Estimation/UKFUpdate Common: Estimation/UKFWeight Common: General/CellToMat Common: General/DeleteCell Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Common: Time/JDToMidnight Math: Integration/RK4 Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
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