Path: SC/Attitude
% Simulate a rhumb line precession. Since version 1. -------------------------------------------------------------------------- Form: [rA, dec, beta] = RLPMnvr( uSun, rAI, decI, azimuth, prec, n ) -------------------------------------------------------------------------- ------ Inputs ------ uSun (3,1) Sun Vector rAI (1,1) Initial right ascension (rad) decI (1,1) Initial declination (rad) azimuth (1,1) Maneuver azimuth (rad) prec (1,1) Precession/pulse (rad) n (1,1) Number of pulses ------- Outputs ------- rA (n+1) Right Ascension (rad) dec (n+1) Declination (rad) beta (n+1) Sun angles (rad) --------------------------------------------------------------------------