Path: SC/Environs
% Computes the normalized sun intensity for an earth geosynchronous orbit. -------------------------------------------------------------------------- Form: [n, eclipseType] = GeoEclps( alpha, beta, dEarth ) -------------------------------------------------------------------------- ------ Inputs ------ alpha (1,1) Angle in the orbit plane between the sun and the spacecraft ( 0 to 2 pi radians ) beta (1,1) Angle between the sun vector and the orbit plane ( -0.409 < beta < 0.409 radians for zero inclination ) dEarth (1,1) Distance to the earth. If not entered assumes 42167 km ------- Outputs ------- n (1,1) Normalized sun intensity ( 0 ? n ? 1 ) eclipseType (1,1) 0 = none, 1 = partial, 2 = annular, 3 = total --------------------------------------------------------------------------
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