FMagSim:

Path: SC/DemoFuns

% Dynamics of spacecraft with one reaction wheel.
 Used by FMagSim2 and FMagSimWithEstimator.
--------------------------------------------------------------------------
   Form:
   xDot = FMagSim( x, t, inr, invInr, tExt, inrW, uW, tW, eSAC )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   x            (8,1)     The state vector
   t            (1,1)     Time (unused)
   inr          (3,3)     Inertia
   invInr       (3,3)     Inverse inertia
   tExt         (3,1)     External torque
   inrW         (1,1)     RWA inertia
   uW           (3,1)     RWA unit vector
   tW           (1,1)     RWA torque

   -------
   Outputs
   -------
   xDot         (15,1)    The derivative of the state vector

   See also QIToBDot, GSModel
--------------------------------------------------------------------------

Children:

AerospaceUtils: Coord/QIToBDot
SC: Dynamics/GSModel
Common: Control/C2DZOH
Math: Linear/Cross
Math: Linear/SkewSymm

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