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Path: SpacecraftEstimation/Demos/StellarAttDet
% Test a star sensor attitude determination system. This system does not use 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 AttDetNoGyros, StarSensor, QMult, QPose, QUnit, Plot2D, RK4, RandSC -------------------------------------------------------------------------- % -------------------------------------------------------------------------- Copyright 1998, 2017 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since version 3. 2017.1 Made compatible with StarIDPyramid. --------------------------------------------------------------------------
Common: Graphics/Plot2D Common: Graphics/TimeLabl Common: Quaternion/QMult Common: Quaternion/QPose Common: Quaternion/QUnit Math: Integration/RK4 SpacecraftEstimation: StellarAttDet/StarIDPyramid SpacecraftEstimation: StellarAttDet/StellarAttDetEKFNoGyros SpacecraftEstimation: StellarCatalog/RandSC SpacecraftEstimation: StellarCatalog/StarDataGeneration SpacecraftEstimation: StellarModels/FRBwRIG SpacecraftEstimation: StellarModels/StarSensor
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