NSSC OpenIR  > 空间环境部
Alternative TitleSpacecraft Potential Control and Potential Monitor During Spacecraft Docking
关燚炳; 王世金; 梁金宝; 刘超; gyb@nssc.ac.cn; wsj@nssc.ac.cn
Source Publication科技导报
Keyword航天器 交汇对接 等离子体 朗缪尔探针
Other AbstractThe different potential between two low orbit spacecrafts is a serious safety problem for the spacecraft docking.The charging mechanism of the spacecraft in the ionosphere plasma is analyzed, and the equivalent circuit model in physics is educed.Based on that, the active potential control method for the International Space Station(ISS) is analyzed and two different methods that make sure of the spacecraft is immune from different potential are proposed.In the end, the solution for the spacecraft potential monitor including the Langmuir probe and the surface potential monitor during the docking is advanced.
Indexed ByCSCD
Funding Project中国科学院空间科学与应用研究中心
Citation statistics
Cited Times:2[CSCD]   [CSCD Record]
Document Type期刊论文
Corresponding Authorgyb@nssc.ac.cn; wsj@nssc.ac.cn
Recommended Citation
GB/T 7714
关燚炳,王世金,梁金宝,等. 航天器交汇对接电位控制研究与航天器电位监测[J]. 科技导报,2011,29(29):27-31.
APA 关燚炳,王世金,梁金宝,刘超,gyb@nssc.ac.cn,&wsj@nssc.ac.cn.(2011).航天器交汇对接电位控制研究与航天器电位监测.科技导报,29(29),27-31.
MLA 关燚炳,et al."航天器交汇对接电位控制研究与航天器电位监测".科技导报 29.29(2011):27-31.
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