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Path: Orbit/OrbitCoord
% Transform from ECI to Rotating Libration Point Coordinates Generates the transformation matrix from ECI to Rotating Libration Point Coordinates. Neglects perturbations due to other bodies. -------------------------------------------------------------------------- Form: c = ECIToRLP( xS ) -------------------------------------------------------------------------- ------ Inputs ------ xS (6,1) [r;v] of the secondary ------- Outputs ------- c (6,6) Transformation from ECI To RLP --------------------------------------------------------------------------
Common: Time/JD2000 Math: Linear/Cross Math: Linear/Mag Math: Linear/Unit SC: Ephem/MoonV1 SC: Ephem/MoonV2
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