Path: SpacecraftEstimation/StellarAttDet
% Computes an attitude quaternion given a set of measured and cataloged unit vectors. The quaternion transforms from the catalog frame to the reference frame. The solution is found from: uMeas = m*uCatalog m = uMeas*pinv(uCatalog); The number of columns should be >= 3 although 2 columns will give an m that is close to the correct matrix. The routine actually computes m and converts m to q. -------------------------------------------------------------------------- Form: [q, m] = QFromU( uCatalog, uMeas ) -------------------------------------------------------------------------- ------ Inputs ------ uCatalog (3,:) Unit vectors from the catalog uMeas (3,:) Corresponding measured unit vectors ------- Outputs ------- q (4,1) Quaternion from reference m (3,3) Transformation matrix from reference --------------------------------------------------------------------------
Common: Quaternion/Mat2Q Common: Quaternion/Q2Mat Common: Quaternion/QRand Common: Quaternion/QUnit Math: Linear/DupVect Math: Linear/Mag Math: Linear/Orthogonalize Math: Linear/Unit
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