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