Path: FormationFlying/Utility
% Generate an orbit by propagating Keplerian elements with impulsive delta-vs. Since version 7. -------------------------------------------------------------------------- Form: [r, v] = RVOrbGenDV( el, t, dV, dVTime ) -------------------------------------------------------------------------- ------ Inputs ------ elI Elements vector [a,i,W,w,e,M] or structure t Times from 0 to ? (sec) dV Array of 3xN delta-v's to be applied (Hills frame) [km/sec] dVTime Array of 1xN times at which delta-v's are applied [sec] ------- Outputs ------- r Position vectors for times t v Velocity vectors for times t el Times at which r and v are calculated --------------------------------------------------------------------------