Path: Missions/Comsat
% Computes spin precession maneuver data for fuel budgets -------------------------------------------------------------------------- Form: x = SpinDataF( inr, iAxis, cM, dW, thrusters ) -------------------------------------------------------------------------- ------ Inputs ------ inr (1,1) Spin axis inertia iAxis (1,1) Axis of spin change cM (3,1) Center of mass dW (1,1) Delta spin rate thrusters (1,n) Thruster IDs ------- Outputs ------- x (1,12+n) Spin change data --------------------------------------------------------------------------
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