aeromodelhighalpha.m

来自「一段用于飞行器大攻角情况的matlab源程序」· M 代码 · 共 9 行

	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