| 引用本文: | 陈克俊.飞船返回再入制导方法研究.[J].国防科技大学学报,1997,19(6):31-35.[点击复制] |
| Chen Kejun.An Approach to Spacecraft Returning Reentry Guidance[J].Journal of National University of Defense Technology,1997,19(6):31-35[点击复制] |
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| 飞船返回再入制导方法研究 |
| 陈克俊 |
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(国防科技大学 自动控制系 湖南 长沙 410073)
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| 摘要: |
| 本文分析研究了飞船离轨返回制动段的制导方法，提出了一种消除制动段误差对再人点状态参数影响的制动发动机综合关机方法，并对再入段的制导方法进行了分析讨论，最后进行了数值仿真分析，论证了方法的可行性。 |
| 关键词: 飞船，返回，再人，制导 |
| DOI： |
| 投稿日期：1997-03-14 |
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| An Approach to Spacecraft Returning Reentry Guidance |
| Chen Kejun |
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(Department of Automatic Control，NUDT，Changsha，410073)
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| Abstract: |
| In this paper，an approach to spacecraft returning reentry guidance is described. The composite shutdown guidance scheme is put forward in the paper，which is applied to decrease reentry state parameters error caused by retro-error in returning phase. And then，reentry guidance law is studied. Finally，it's correctness is proved by simulation. |
| Keywords: spacecraft,return,reentry,guidance |
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