T_n = 5765;

ws = 2*pi/(365.2422*24*3600);

for j = 1:s_m, tmp(j) = Om_n0+ws*t(j);

end

Om_n = tmp';

clear tmp;

map = [1,1,1];

colormap(map);

plot(t,p,'y-',[min(t) max(t)],[p_n p_n],'r-'), title (' Фокальный параметр '), grid on;

print -dwin;

pause;

plot(t,p-p_n,'y-'), title (' dp '), grid on;

print -dwin;

pause;

plot(t,e,'y-',[min(t) max(t)],[e_n e_n],'r-'), title (' Эксцентриситет '), grid on;

print -dwin;

pause;

plot(t,e-e_n,'y-'), title (' de '), grid on;

print -dwin;

pause;

plot(t,a,'y-',[min(t) max(t)],[a_n a_n],'r-'), title (' Большая полуось орбиты '), grid on;

print -dwin;

pause;

plot(t,a-a_n,'y-'), title (' da '), grid on;

print -dwin;

pause;

plot(t,Om*r_g,'y-',t,Om_n*r_g,'r-'), title (' Долгота восходящего узла '), grid on;

print -dwin;

pause;

plot(t,Om*r_g-Om_n*r_g,'y-'), title (' dOm '), grid on;

print -dwin;

pause;

plot(t,i*r_g,'y-',[min(t) max(t)],[i_n*r_g i_n*r_g],'r-'), title (' Наклонение '), grid on;

print -dwin;

pause;

plot(t,i*r_g-i_n*r_g,'y-'), title (' di '), grid on;

print -dwin;

pause;

plot(t,T,'y-',[min(t) max(t)],[T_n T_n], 'r-'), title (' Период '), grid on;

print -dwin;

pause;

plot(t,T-T_n,'y-'), title (' dT '), grid on;

print -dwin;

pause;

plot3(x,y,z,'b')

axis([min(x) max(x) min(y) max(y) min(z) max(z)])

set(gca,'box','on')

title (' Положение МКА ')

hold on

plt = plot3(0,0,0,'.','erasemode','xor','markersize',24);

dk = ceil(length(y)/2500);

for k = 1:dk:length(y)

set(plt,'xdata',x(k),'ydata',y(k),'zdata',z(k))

drawnow

end

hold off

pause;

plot(t,Fz,'y-'), title (' Гравитация Земли ' ), grid on;

print -dwin;

pause;

plot(t,Fs,'y-'), title (' Гравитация Солнца и солнечное давление '), grid on;

print -dwin;

pause;

plot(t,Fl,'y-'), title (' Гравитация Луны '), grid on;

print -dwin;

pause;

plot(t,Fa,'y-'), title (' Сопротивление атмосферы '), grid on;

print -dwin;

pause;

plot(t,U20,'y-'), title (' Нецентральность гравитационного поля Земли '), grid on;

print -dwin;

pause;

plot(t,Fz+Fs+Fl+Fa+U20,'y-'), title (' Суммарное возмущающее ускорение '), grid on;

print -dwin;

pause;

clear all

clc

g_r = pi/180;

r_g = 180/pi;

p_n = 6952137.;

e_n = 0;

a_n = 6952137.;

Om_n0 = 28.1*g_r;

i_n = 97.6*g_r;

omg_n = 346.725*g_r;

T_n = 5765;

load u_par.dat

t_u = u_par(:,1);

p_u = u_par(:,2);

e_u = u_par(:,3);

a_u = u_par(:,4);

Om_u = u_par(:,5);

i_u = u_par(:,6);

omg_u = u_par(:,7);

T_u = u_par(:,8);

u_u = u_par(:,9);

clear u_par;

load u_f.dat;

Fz_u = u_f(:,2);

Fs_u = u_f(:,3);

Fl_u = u_f(:,4);

Fa_u = u_f(:,5);

U20_u = u_f(:,6);

clear u_f;

s_tmp = size(t_u);

s_m_u = s_tmp(1);

clear s_tmp;

ws = 2*pi/(365.2422*24*3600);

for j = 1:s_m_u, tmp(j) = Om_n0+ws*t_u(j);

end

Om_n_u = tmp';

clear tmp;

plot(t_u,p_u,'y-',[min(t_u) max(t_u)],[p_n p_n],'r-'), title (' Фокальный параметр '), grid on;

print -dwin;

pause;

plot(t_u,p_u-p_n,'y-'), title (' dp '), grid on;

print -dwin;

pause;

plot(t_u,e_u,'y-',[min(t_u) max(t_u)],[e_n e_n],'r-'), title (' Эксцентриситет '), grid on;

print -dwin;

pause;

plot(t_u,e_u-e_n,'y-'), title (' de '), grid on;

print -dwin;

pause;

plot(t_u,a_u,'y-',[min(t_u) max(t_u)],[a_n a_n],'r-'), title (' Большая полуось орбиты '), grid on;

print -dwin;

pause;

plot(t_u,a_u-a_n,'y-'), title (' da '), grid on;

print -dwin;

pause;

plot(t_u,Om_u*r_g,'y-',t_u,Om_n_u*r_g,'r-'), title (' Долгота восходящего узла '), grid on;

print -dwin;

pause;

plot(t_u,Om_u*r_g-Om_n_u*r_g,'y-'), title (' dOm '), grid on;

print -dwin;

pause;

plot(t_u,i_u*r_g,'y-',[min(t_u) max(t_u)],[i_n*r_g i_n*r_g],'r-'), title (' Наклонение '), grid on;

print -dwin;

pause;

plot(t_u,i_u*r_g-i_n*r_g,'y-'), title (' di '), grid on;

print -dwin;

pause;

plot(t_u,T_u,'y-',[min(t_u) max(t_u)],[T_n T_n], 'r-'), title (' Период '), grid on;

print -dwin;

pause;

plot(t_u,T_u-T_n,'y-'), title (' dT '), grid on;

print -dwin;

pause;

clear all