Path: SpacecraftEstimation/OrbitEstimation
% Demonstrate orbit estimation using UKFPredict and UKFUpdate. The plots are the covariance, which goes to zero quickly, and the estimation errors. It uses GPS and single Doris range rate sensor. See also KFInitialize, RK4, UKFPredict, UKFUpdate, RHSOrbitWithDisturbances, UKFWeight, MeasEarthTarget, MeasOrbitState
SC: BasicOrbit/RHSOrbit SC: Ephem/EOfE SC: Ephem/EarthRot SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/NutDelta SC: Ephem/ObOfE SpacecraftEstimation: OrbitEstimation/MeasDoris SpacecraftEstimation: OrbitEstimation/MeasOrbitState Common: CommonData/SwooshWatermark Common: Estimation/KFInitialize Common: Estimation/UKFPredict Common: Estimation/UKFUpdate Common: Estimation/UKFWeight Common: General/CellToMat 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/Skew Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/CosD Math: Trigonometry/SinD
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