Path: ACPro/ACPerformance
% Computes the angle of attack for a constant flight path angle.
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Form:
alpha = ComputeAlphaConstantFlightPathAngle( x, d )
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Inputs
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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
.atmData (.) Data structure
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Outputs
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alpha (1,1) Angle of attack
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ACPro: ACPointMass/SimpleLiftAndDrag AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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