Path: Missions/SunNadir
% Compute the orbit right ascension angle 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. -------------------------------------------------------------------------- Form: rA = SunRA( i, uSun, beta ) -------------------------------------------------------------------------- ------ 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) --------------------------------------------------------------------------
AerospaceUtils: Coord/U2RADec Common: Graphics/Plot2D
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