| 引用本文: | 张进,李海阳,罗亚中,等.远程导引变轨故障后轨道重构设计与分析.[J].国防科技大学学报,2009,31(6):50-56.[点击复制] |
| ZHANG Jin,LI Haiyang,LUO Yazhong,et al.The Orbital Reconfiguring Design and Analysis after Maneuver Failure for Rendezvous Phasing[J].Journal of National University of Defense Technology,2009,31(6):50-56[点击复制] |
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| 远程导引变轨故障后轨道重构设计与分析 |
| 张进, 李海阳, 罗亚中, 唐国金 |
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(国防科技大学 航天与材料工程学院，湖南 长沙 410073)
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| 摘要: |
| 研究了空间交会远程导引变轨故障后轨道重构问题，提出了轨道重构设计准则，对五冲量远程导引的每一次变轨故障分别给出了四类轨道重构方案。根据提出的设计准则对给出轨道重构方案的修正能力、测控条件、推进剂消耗、终端精度和安全性进行初步分析，确定了处理远程导引变轨故障的轨道预案。 |
| 关键词: 空间交会 远程导引 变轨故障 轨道机动 轨道重构 |
| DOI： |
| 投稿日期：2009-04-30 |
| 基金项目:国家自然科学基金资助项目(10902121)；中国博士后科学基金资助项目(20090450210)；国防科技大学科研计划资助项目(JC09-01-01) |
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| The Orbital Reconfiguring Design and Analysis after Maneuver Failure for Rendezvous Phasing |
| ZHANG Jin, LI Haiyang, LUO Yazhong, TANG Guojin |
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(College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China)
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| Abstract: |
| The orbital reconfiguring problem after maneuver failure for rendezvous phasing is studied. The orbital reconfiguring design rules are proposed and four types of orbital reconfiguring plan are provided respectively for every maneuver failure in five-impulse phasing mission. Based on the proposed design rules, the provided reconfiguring plan's correcting ability, tracking and command condition, propellant consumed, terminal precision and security are analyzed. Finally, the orbital counter plan to deal with rendezvous phasing maneuver failure is obtained. |
| Keywords: space rendezvous phasing maneuver failure orbital maneuver orbital reconfiguring |
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