?? aeromodelhighalpha.m
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function [CD,CL,CY,Cl,Cm,Cn,Thrust] = AeroModel(x,u,Mach,alphar,betar,V)% Aerodynamic Coefficients of the Aircraft, Thrust Model,% and Geometric and Inertial Properties% July 2, 2002% Business Jet -- High-Angle-of-Attack, Mach-Independent Model% Landing Gear: Up (GEAR = 0)% Flap Setting, u(6): 0?? 快捷鍵說明
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