RHSSNP:

Path: Missions/SunNadir

% Spacecraft sun-nadir RHS with 4 RWA's and 2 solar arrays.
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   Form:
   xDot = RHSSNP( x, t, inr, invInr, tExt, inrW, uW, tW, eSAC )
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   ------
   Inputs
   ------
   x            (15,1)    The state vector
   t                      Time
   inr          (3,3)     Inertia
   invInr       (3,3)     Inverse inertia
   tExt         (3,1)     External torque
   inrW         (6)       [SA,RWA] inertias
   uW           (3,6)     [SA,RWA] unit vectors
   tW           (6)       [SA,RWA] torque
   eSAC         (2)       Solar array commanded angle (always one step)

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

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  See also GSModel, SunNadirPointingSim
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Children:

AerospaceUtils: Coord/QIToBDot
SC: Dynamics/GSModel

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