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SUPPORT SITE |
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Path: Orbit/OrbitControl
% Low thrust control. -------------------------------------------------------------------------- Form: accel = LowThrustControl( r, v, accel, mu ) -------------------------------------------------------------------------- ------ Inputs ------ r (3,1) Position v (3,1) Velocity accel (1,1) Scalar disturbance acceleration mu (1,1) Gravitational parameter ------- Outputs ------- accel (3,1) Vector acceleration --------------------------------------------------------------------------
AerospaceUtils: Coord/QLVLH Common: Quaternion/QTForm Math: Linear/Mag SC: BasicOrbit/RV2El
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