Path: FormationFlying/Transformation
% Compute standard differential elements from Alfriend differential elements. Since version 7. -------------------------------------------------------------------------- Usage: [dEl,T] = DeltaEl2Alfriend( e, w, M, dElA ); -------------------------------------------------------------------------- ------ Inputs ------ e (1) Eccentricity w (1) Argument of perigee [rad] M (1) Mean anomaly [rad] dElA (1,6) Orbital element differences [a,th,i,q1,q2,W] ------- Outputs ------- dEl (1,6) Orbital element differences [a,i,W,w,e,M] T (6,6) Transformation matrix --------------------------------------------------------------------------