transmaov.m

matlab实现的卫星轨道模拟

function Aov=TransMaov(Upw,Orbit_i,Nearw)
Aov1=[
        cos(Upw)   -sin(Upw)   0;
        sin(Upw)   cos(Upw)    0;
           0          0        1;
     ];
Aov2=[
           1          0           0;
           0   cos(Orbit_i)  -sin(Orbit_i);
           0   sin(Orbit_i)  cos(Orbit_i);
     ];
Aov3=[
           cos(Nearw)   -sin(Nearw)   0;
           sin(Nearw)   cos(Nearw)    0;
               0            0         1;
     ];
Aov=Aov1*Aov2*Aov3;