Path: SpacecraftEstimation/StellarAttDet
% Propagates a quaternion one step Assuming that the angular velocity is constant. ------------------------------------------------------------------------ Form: q = AttProp( w, q, dT ) ------------------------------------------------------------------------ ------ Inputs ------ w (3,1) Angular velocity q (4,1) Old quaternion dT (1,1) Time change ------- Outputs ------- q (4,1) Updated quaternion ------------------------------------------------------------------------
Common: Quaternion/QUnit Math: Linear/DupVect Math: Linear/Mag Math: Linear/SkewSymm
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