Path: SpacecraftEstimation/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 Version 2018.1 Added RIG noise to the simulation. --------------------------------------------------------------------------