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