ACEngEq:

Path: AC/Aircraft

% Find the equilibrium state of the engine.
   Since version 2 (ACT)
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   Form:
   x = ACEngEq( d, v, r )
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   ------
   Inputs
   ------
   d                     Aircraft data
   v              (3,1)  Velocity
   r              (3,1)  Position

   -------
   Outputs
   -------
   x                     Equilibrium engine state

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   See also Altitude, AirData, ACEngine
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Children:

AC: Aircraft/ACEngine
AerospaceUtils: AtmosphericCalculations/AirData
Common: Transform/Altitude
Math: Linear/Mag

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