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远程导引变轨故障后轨道重构设计与分析
引用本文:张进,李海阳,罗亚中,唐国金.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.
作者姓名:张进  李海阳  罗亚中  唐国金
作者单位:国防科技大学航天与材料工程学院,湖南,长沙,410373
基金项目:国家自然科学基金,中国博士后科学基金,国防科技大学科研计划 
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
收稿时间:2009/4/30 0:00:00

The Orbital Reconfiguring Design and Analysis after Maneuver Failure for Rendezvous Phasing
ZHANG Jin,LI Haiyang,LUO Yazhong and TANG Guojin.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.
Authors:ZHANG Jin  LI Haiyang  LUO Yazhong and TANG Guojin
Institution:ZHANG Jin,LI Hai-yang,LUO Ya-zhong,TANG Guo-jin (College of Aerospace and Material Engineering,National Univ.of Defense Technology,Changsha 410073,China)
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 rendezvou...
Keywords:space rendezvous  phasing  maneuver failure  orbital maneuver  orbital reconfiguring
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