Path: Missions/Comsat
% Generates the data needed for initialization in TransferOrbit.m -------------------------------------------------------------------------- Form: x = IntData( elements, rA, dec, w, hW, fuelMass ) -------------------------------------------------------------------------- ------ Inputs ------ elements (1,6) Keplerian elements rA (1,1) Right ascension (deg) dec (1,1) Declination (deg) w (3,1) Spin vector (rad/sec) hW (1,1) Wheel momentum fuelMass (1,n) Fuel mass (per tank) (lbf) ------- Outputs ------- x (1,8+n) Formatted data --------------------------------------------------------------------------
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