Оптимизация траектория космического аппарата с помощью идеально-регулируемого двигателя в окрестности круговой орбиты
Table 1 - Results of calculating the components of velocity impulses for two and three-channel control
t | ∆Vx2 * 10-3 | ∆Vy2 * 10-3 | ∆Vz2 * 10-3 | ∆Vx3 * 10-3 | ∆Vy3 * 10-3 | ∆Vz3 * 10-3 |
0 | -0.131 | 1.313 | 0.394 | -0.131 | 1.313 | 0.394 |
1.064 | 4.784 | -5.948 | 0.751 | 4.731 | -5.799 | 0.751 |
2.128 | 2.807 | -16 | 0.333 | 2.781 | -16 | 0.333 |
3.192 | -3.1 | -16 | -0.345 | -3.054 | -16 | -0.345 |
4.256 | -6.443 | -5.41 | -0.583 | -6.361 | -5.462 | -0.583 |
5.32 | -4.132 | 6.083 | -0.224 | -4.082 | 5.909 | -0.224 |
6.384 | 0.874 | 8.647 | 0.28 | 0.872 | 8.526 | 0.28 |
7.448 | 3.425 | 2.606 | 0.415 | 3.377 | 2.625 | 0.415 |
8.512 | 1.596 | -3.556 | 0.13 | 1.574 | -3.477 | 0.13 |
9.576 | -1.806 | -3.026 | 0.0372 | -1.78 | -3.032 | 0.0372 |
10.64 | -2.942 | 2.788 | -0.2465 | -2.9 | 2.646 | -0.2465 |
11.704 | -1.046 | 7.247 | -0.051 | -1.031 | 7.066 | -0.051 |
12.768 | 1.385 | 6.358 | 0.107 | 1.359 | 6.272 | 0.107 |
13.832 | 1.901 | 2.347 | 0.0797 | 1.861 | 2.386 | 0.0797 |
14.896 | 0.749 | -0.191 | -0.0126 | 0.727 | -0.121 | -0.0126 |
15.963 | 1.687* 10-7 | 3.514* 10-4 | -3.358* 10-5 | 6.614* 10-6 | 3.111* 10-4 | -3.358* 10-5 |