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Path: SpacecraftEstimation/StellarAttDet
% Computes the state transition matrix for the delta quaternion only. Since version 3. ------------------------------------------------------------------------ Form: phi = DSTMQ( w, dT ) ------------------------------------------------------------------------ ------ Inputs ------ w (3,1) Nominal rate dT (1,1) Time step ------- Outputs ------- phi (3,3) State transition matrix ------------------------------------------------------------------------
Math: Linear/SkewSymm
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