FPivot:

Path: SC/Dynamics

% Computes the right hand side of the spacecraft with pivot eofm.

   Since version 1.
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   Form:
   xDot = FPivot( x, t, jW, jP, iS, tS, tW, tP, uW, uP, pivotC )
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   ------
   Inputs
   ------
   x           (10,1)  State vector [q;theta;w(3,1);wP;wW]
   t           (1,1)   Time
   jW          (3,3)   Wheel inertia (must be symmetric)
   jP          (3,3)   Pivot assembly inertia
   iS          (3,3)   Spacecraft inertia
   tS          (3,1)   Body torque
   tW          (1,1)   Wheel torque
   tP          (1,1)   Pivot torque
   uW          (3,1)   Wheel axis
   uP          (3,1)   Pivot axis
   pivotC      (1,1)   Commanded pivot angle

   -------
   Outputs
   -------
   xDot        (10,1)  Time derivative

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Children:

AerospaceUtils: Coord/QIToBDot
SC: Dynamics/SCwPivot

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