myfly.m

飞行控制问题

clear;
clc;
tic;
global  x y theata0 theta delta_x delta_y c s b d_theta t z;
ub=[30 30 30 30 30 30];
lb=-ub;
x0=[0.5 0.1 0.1 0.3 0.4 0.23];
[x,fval,exitflag,output]=fmincon(@fly,x0,[],[],[],[],lb,ub,@noncon)
toc;