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SUPPORT SITE |
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SUPPORT SITE |
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Path: SC/Dynamics
% Spacecraft with multiple wires
Since version 2.
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Form:
xDot = WireFRB( x, t, s, mu, torque, force )
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Inputs
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x (m,1) The state vector
[x;v;q;w;xWire;vWire]
t Time
s (:) Wire data structure
mu (1,1) Gravitational parameter
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Outputs
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xDot (m,1) The derivative of the state vector
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AerospaceUtils: Coord/QIToBDot Common: Quaternion/QForm Math: Linear/Cross Math: Linear/Mag Math: Linear/SkewSq Math: Linear/SkewSymm Math: Linear/Unit
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