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Path: SpacecraftEstimation/Demos/StellarAttDet
% Simulate a star sensor attitude determination system with gyros. dT is the time step for the attitude determination system. You can numerically integrate with a smaller time step by setting nInt > 1. ------------------------------------------------------------------------- See also StellarAttDetUKF, StarDataGeneration, StarSensor and RandSC -------------------------------------------------------------------------
Common: Graphics/Plot2D Common: Graphics/TimeLabl Common: Quaternion/QMult Common: Quaternion/QPose Common: Quaternion/QUnit Math: Integration/RK4 SC: Sensor/RIGOut SpacecraftEstimation: StellarAttDet/StarIDPyramid SpacecraftEstimation: StellarAttDet/StellarAttDetUKF SpacecraftEstimation: StellarCatalog/RandSC SpacecraftEstimation: StellarCatalog/StarDataGeneration SpacecraftEstimation: StellarModels/FRBwRIG SpacecraftEstimation: StellarModels/StarSensor
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