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- W2539132007 abstract "Orbit maneuver exhibits significant applications in formation flight, spacecraft information supporting and on-orbit servicing etc. In the paper, we pay more attention to analyze spacecraft's control domain under extra maneuver ability. According to emulate different direction velocity increment in different plane thrown to spacecraft, we analyze the variation of orbit parameters change with velocity increment. Furthermore, we give some conclusions which can provide theory foundation for the task of spacecraft information supporting and on-orbit servicing." @default.
- W2539132007 created "2016-10-28" @default.
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- W2539132007 date "2014-08-01" @default.
- W2539132007 modified "2023-09-28" @default.
- W2539132007 title "Emulation and analysis of spacecraft control domain" @default.
- W2539132007 cites W2114799916 @default.
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- W2539132007 doi "https://doi.org/10.1109/cgncc.2014.7007349" @default.
- W2539132007 hasPublicationYear "2014" @default.
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