Path: Orbit/OrbitCoord
% Computes the differences between orbital element vectors.
This wraps the phase appropriately for all the angular elements.
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Form:
dEl = OrbElemDiff( el0, el, type )
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Inputs
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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] (default)
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Outputs
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dEl (:,6) orbital element differences
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Math: Trigonometry/WrapPhase
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