HGimballedBoom:

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   Calculate angular momentum of boom system and update the body rates.

   Since version 7.
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   Form:
   [hI, hW] = HGimballedBoom( x, g, axis, aDotNew, hW )
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   Inputs
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   x             (15,1)   The state vector [r;v;q;omega;a;aDot]
   g             (1,1)    CAD model
   axis          (3,2)    Rotation axes of gimbals
   aDotNew       (2,1)    New gimbal rates
   hW            (3,1)    Stored angular momentum

   -------
   Outputs
   -------
   hI            (3,1)    Inertial angular momentum
   hW            (3,1)    Updated stored momentum

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Children:

Common: Quaternion/QForm
Common: Quaternion/QTForm
Math: Linear/Cross
Math: Linear/Skew
Math: Linear/SkewSq
Sail: Disturbances/HingeRotationMatrix