FCoreAndMoving:

--------------------------------------------------------------------------
   Example system RHS which incorporates FMovingBody.
   The orbit states have a zero derivative. Loops through the n bodies
   and performs attitude kinematics on each.

   Since version 7.
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   Form:
   vargout = FCoreAndMoving( t, x, flag, d )
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   ------
   Inputs
   ------
   t                      Time (s)
   x             (:,1)    The state vector, [r;v;q;w;...]
   flag          (1,:)    Flags for ode113
   d             (1,1)    Data structure for FMovingBody
                           .g
                           .force
                           .torque

   -------
   Outputs
   -------
   xDot          (:,1)     The state vector derivative

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

Children:

AeroUtils: Coord/QIToBDot
Sail: AttitudeDynamics/FMovingBody