run_accelclimb.m

大气层内航天器飞行动力学matlab仿真模型

% Copyright Ashish Tewari (c) 2006
global dtr; dtr = pi/180;
global mu; mu = 3.986004e14;  
global omega; omega = 2*pi/(23*3600+56*60+4.0905); 
global S; S =  56.5;  
global c; c=3.9926; 
global rm; rm = 6378140 ;  
global b; b=14.1512; 
global CLmax; CLmax=1.5;
global sweep; sweep=50*pi/180; 
global f8; f8 = fopen('data8.mat', 'a');
long =70*dtr;       
lat = 20*dtr;       
radint=rm+200;     
velint=69;         
fpaint=40*dtr;     
chiint=270*dtr;    
m=17350;           
options=odeset('RelTol',1e-4);
init = [long; lat; radint; velint; fpaint; chiint; m]; 
[t, o] = ode45('accelclimb',[0, 80], init,options);
fclose('all');