SunRA:

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   Computes the orbit right ascension angle
   given the sun unit vector (or right ascension and declination),
   the sun beta angle and the inclination of the orbit.

   Type SunRA for a demo.

   Since version 1.
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   Form:
   rA = SunRA( i, uSun, beta )
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   Inputs
   ------
   i            (1,1)  Inclination (rad)
   uSun         (3,1)  Sun Vector or [rASun (rad);decSun (rad)];
   beta         (1,n)  Beta angles (rad)

   -------
   Outputs
   -------
   rA           (1,n)  Right ascension of the ascending node (rad)

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Children:

AeroUtils: Coord/U2RADec
Common: Graphics/Plot2D