ComputeAlphaConstantFlightPathAngle:

Path: ACPro/ACPerformance

% Computes the angle of attack for a constant flight path angle.

   Since version 8.
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   Form:
   alpha = ComputeAlphaConstantFlightPathAngle( x, d )
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   ------
   Inputs
   ------
   x          (4,1)   [v;gamma;h;m]
   d           (.)    Data structure
                      .aero     (.) Aero data structure
                      .cDCL    (1,1) Pointer to lift and drag function
                      .thrust  (1,1) Thrust

   -------
   Outputs
   -------
   alpha      (1,1)   Angle of attack

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Children:

Common: Atmosphere/StdAtm

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