DeltaElem2Hills:
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Computes the Hills frame state from orbital element differences and
reference orbital elements.
Since version 7.
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Usage:
[xH,m] = DeltaElem2Hills( el0, dEl, J2 );
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Inputs
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el0 (1,6) reference orbital elements: [a,th,i,q1,q2,W]
dEl (:,6) orbital element differences: [a,th,i,q1,q2,W]
J2 (1) size of the J2 perturbation
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Outputs
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xH (6,:) relative position and velocity in Hills frame [km; km/s]
m (6,6) transformation matrix
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Children:
FormationFlying: Transformation/Hills2DeltaElem
