Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (22): 330196.doi: 10.7527/S1000-6893.2024.30196
• Electronics and Electrical Engineering and Control • Previous Articles
Lu BAI1, Defu LIN1, Duo ZHENG1(), Mingjun WEI2
Received:
2024-01-19
Revised:
2024-03-21
Accepted:
2024-05-06
Online:
2024-05-28
Published:
2024-05-22
Contact:
Duo ZHENG
E-mail:zhengduohello@126.com
Supported by:
CLC Number:
Lu BAI, Defu LIN, Duo ZHENG, Mingjun WEI. Guidance technology of specified direction and attitude for plane symmetrical aircraft with directed energy load constraint[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(22): 330196.
Table 7
Simulation results analysis of constraints in multiple target situation
约束项 | 目标 | 目标 | 目标 | 要求 | |
---|---|---|---|---|---|
期望值 | 9.48 | -13.48 | 4.48 | 满足 | |
实际值 | 9.63 | -13.58 | 4.58 | ||
偏差值 | 0.15 | -0.10 | 0.10 | ||
期望值 | 0 | 0 | 0 | 满足 | |
实际值 | 0.10 | 0.09 | -0.01 | ||
偏差值 | 0.10 | 0.09 | -0.01 | ||
期望值 | -15 | 10 | -5 | 满足 | |
实际值 | -14.95 | 10.01 | -5 | ||
偏差值 | 0.05 | 0.01 | 0 | ||
期望值 | 500 | 100 | 600 | 满足 | |
实际值 | 499.73 | 99.81 | 600.31 | ||
偏差值 | -0.27 | -0.19 | 0.31 |
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