Path: SpacecraftEstimation/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. --------------------------------------------------------------------------