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System design and principle analysis of stratospheric satellite

  • Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节会议稿件同行评审

4 引用 (Scopus)

摘要

A stratospheric satellite is a new kind of aerostat, and consists of stratosail, superpressure helium balloon, tether and energy system. It flies around the earth from east to west in the stratosphere at the altitude 35 km, and its flight from north to south can be controlled by the traction of the stratosail. In this paper, we analyze the wind field of the stratosphere and present the trajectory control principle of the stratospheric satellite, establish the model of stratospheric satellite and simulate its control system of the stratospheric satellite from north to south. The simulation results show that the control system can achieve the steady control.

源语言英语
主期刊名International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008
2867-2873
页数7
出版状态已出版 - 2008
活动59th International Astronautical Congress 2008, IAC 2008 - Glasgow, 英国
期限: 29 9月 20083 10月 2008

出版系列

姓名International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008
5

会议

会议59th International Astronautical Congress 2008, IAC 2008
国家/地区英国
Glasgow
时期29/09/083/10/08

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