ASim:

Path: SC/Dynamics

% Attitude simulation of a rigid body.

   Since version 1.
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   Form:
   xDot = ASim( x, t, inertia, torque )
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   ------
   Inputs
   ------
   x           (7,1)     [Attitude quaternion; attitude rate]
   t                     Time
   inertia     (3,3)     Inertia matrix
   torque      (3,1)     External torque

   -------
   Outputs
   -------
   xDot        (7,1)     Derivative of the state, x

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Children:

AerospaceUtils: Coord/QIToBDot
SC: Dynamics/RBModel

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