Path: Orbit/OrbitPropagator
% Computes the engine force vector in the ECI frame.
The input is in the LVLH frame.
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Form:
x = FEngine( action, modifier, u, t )
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Inputs
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action (1,:) Action 'initialize', 'update'
modifier (1,:) Modifier to the action or data structure if initialization
u (7,1) [r;v;m]
t (1,1) Time
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Outputs
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x (1,1) The tag if action is 'initialize'
If the action is update
x.f (3,1) Force vector in the ECI frame
x.mDot (1,1) Mass derivative
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AerospaceUtils: Coord/QLVLH Orbit: OrbitPropagator/PropagateOrbitPlugIn Common: General/CloseFigure Common: Help/HelpSystem Common: Quaternion/QTForm
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