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Path: SpacecraftEstimation/Demos/StellarAttDet
% Test 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 StellarAttDetEKF, StarDataGeneration, StarSensor and RandSC ------------------------------------------------------------------------- % -------------------------------------------------------------------------- Copyright (c) 2016 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since version 2017.1 --------------------------------------------------------------------------
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/StellarAttDetEKF SpacecraftEstimation: StellarCatalog/RandSC SpacecraftEstimation: StellarCatalog/StarDataGeneration SpacecraftEstimation: StellarModels/FRBwRIG SpacecraftEstimation: StellarModels/StarSensor
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