Attitude determination system for nano-satelite
The thesis focuses on the attitude determination system of a satellite. Attitude determination is the process of computing the spacecraft orientation relative to inertial reference frame such as the Earth center inertial frame. The attitude determination process is critical in satellite operation...
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| 格式: | Theses and Dissertations |
| 語言: | English |
| 出版: |
2014
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/60707 |
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| 機構: | Nanyang Technological University |
| 語言: | English |