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Attitude determination and control of LEO microsatellites

The Attitude Determination and Control System algorithm and code have been developed and tested for the possible use in the proposed X-Sat, a LEO microsatellite of NTU. The X-Sat is currently under development and is expected to be launched in 2005 into a circular orbit at a height of 800km. An Equa...

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書目詳細資料
主要作者: Wee, Melisa Toon Cheng.
其他作者: Arichandran, K.
格式: Theses and Dissertations
出版: 2008
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在線閱讀:http://hdl.handle.net/10356/3724
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