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