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Path: Orbit/OrbitCoord
% Find the relative coordinate state vector between x2 and x1. This function is consistent with Hill's equations. -------------------------------------------------------------------------- Form: [d, y, z] = RelativeOrbitState( x1, x2 ) -------------------------------------------------------------------------- ------ Inputs ------ x1 (6,1) [r;v] x2 (6,1) [r;v] ------- Outputs ------- d (6,1) [dR;r1*dTheta;dZ;dRDot;r1*dThetaDot;dZDot] y (3,1) Tangent vector --------------------------------------------------------------------------
Math: Linear/Cross Math: Linear/Mag Math: Linear/Unit
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