Path: AerospaceUtils/Coord
% Computes right ascension and declination and their rates. Type RVToRADec for a demo. -------------------------------------------------------------------------- Form: [rA, dec, rADot, decDot] = RVToRADec( r, v ) -------------------------------------------------------------------------- ------ Inputs ------ r (3,n) Position vectors v (3,n) Velocity vectors ------- Outputs ------- rA (1,n) Right ascension dec (1,n) Declination rADot (1,n) Right ascension rate decDot (1,n) Declination rate --------------------------------------------------------------------------