Path: FormationFlying/Transformation
% Computes the Hills frame state from orbital element differences and reference orbital elements. -------------------------------------------------------------------------- Usage: [xH,m] = DeltaElem2Hills( el0, dEl, J2 ); -------------------------------------------------------------------------- ------ Inputs ------ 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 ------- Outputs ------- xH (6,:) relative position and velocity in Hills frame [km; km/s] m (6,6) transformation matrix --------------------------------------------------------------------------
FormationFlying: Transformation/Hills2DeltaElem
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