WireFRB:

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

--------------------------------------------------------------------------

Children:

AerospaceUtils: Coord/QIToBDot
Common: Control/C2DZOH
Common: Quaternion/QForm
Math: Linear/Cross
Math: Linear/Mag
Math: Linear/SkewSq
Math: Linear/SkewSymm
Math: Linear/Unit

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