AB2RADec:

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.
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   Form:
   [rA, dec] = AB2RADec( i, L, w, alpha, beta )
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   ------
   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

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Children:

AerospaceUtils: Coord/U2RADec
Common: Transform/RaDec2U
SC: BasicOrbit/CP2I

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