Path: Orbit/OrbitCoord
% Computes the differences between orbital element vectors. This wraps the phase appropriately for all the angular elements. -------------------------------------------------------------------------- Form: dEl = OrbElemDiff( el0, el, type ) -------------------------------------------------------------------------- ------ Inputs ------ el0 (1,6) reference orbital elements el (1,6) secondary orbital elements type (1) type 1 -- [a,th,i,q1,q2,W] 2 -- [a,i,W,w,e,M] ------- Outputs ------- dEl (:,6) orbital element differences --------------------------------------------------------------------------
Math: Trigonometry/WrapPhase
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