AircraftControlCAS:

Path: AC/ACControl

% Implements a pitch rate control augmentation system.
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   Form:
   y = AircraftControCAS( action, d )
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   ------
   Inputs
   ------
   action         (1,:)       Action for function
   d              (:)         Input

   -------
   Outputs
   -------
   y              (1,1)       Output depends on action

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Children:

Common: Control/C2DZOH

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