摘要
Accounting for the requirement of the terminal angular constraint of video-guided penetration bomb, a guidance law based on variable-structure backstepping method was derived. Through computer simulation, the influence of the guidance law parameters on the guidance performance was discussed. The effect of the guidance law was tested under the conditions of different release method and expected impact angle. The result showed the effectiveness and robustness of the guidance law.
源语言 | 英语 |
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页(从-至) | 208-214 |
页数 | 7 |
期刊 | Yuhang Xuebao/Journal of Astronautics |
卷 | 29 |
期 | 1 |
出版状态 | 已出版 - 1月 2008 |