FAKM:

Path: SC/Dynamics

% AKM Burn right-hand-side

   Since version 1.
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   Form:
   xDot = FAKM( x, t, inr, inrDot, mRDot, hMWA, inrDamper, cDamper, uDamper, tAKM, tBurn )
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   ------
   Inputs
   ------
   x            (8,1)     The state vector
   t            (1,1)     Time
   inr          (3,3)     Inertia
   inrDot       (3,3)     Inertia derivative
   mRDot        (3,3)     Jet damping term
   hMWA         (3,1)     Wheel momentum vector
   inrDamper    (1,1)     Damper wheel inertia
   cDamper      (1,1)     Damper damping coefficient
   uDamper      (3,1)     Damper unit vector
   tAKM         (3,1)     AKM torque
   tBurn        (1,1)     Burn duration

   -------
   Outputs
   -------
   xDot         (8,1)     The derivative of the state state vector

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Children:

AerospaceUtils: Coord/QIToBDot
Math: Linear/Cross

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