Path: Orbit/OrbitCoord
% Right ascension and declination with their rates from position and velocity vectors. You can just enter r to get just rA and dec. -------------------------------------------------------------------------- Form: [rA, dec, rARate, decRate] = RV2RaDec( r, v ) -------------------------------------------------------------------------- ------ Inputs ------ r (3,n) Position vectors v (3,n) Velocity vectors ------- Outputs ------- rA (1,n) Right ascension dec (1,n) Declination rARate (1,n) Right ascension rate decRate (1,n) Declination rate --------------------------------------------------------------------------
Math: Linear/Dot Math: Linear/Mag Math: Linear/Unit
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