Path: Orbit/OrbitCoord
% Convert angles to right ascension and declination Converts angles in the orbit plane to right ascension and declination in the ECI frame. -------------------------------------------------------------------------- Form: [rA, dec] = AB2RADec( i, L, w, alpha, beta ) -------------------------------------------------------------------------- ------ Inputs ------ i Inclination L Longitude of the ascending node w Argument of perigee alpha Angle of the vector with respect to perigee beta Angle of the vector with respect to the orbit plane ------- Outputs ------- rA Right ascension in the ECI frame dec Declination of the ECI fram --------------------------------------------------------------------------
AerospaceUtils: Coord/U2RADec SC: BasicOrbit/CP2I Common: Transform/RaDec2U
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