Attitude control simulation of small satellites with reaction wheels
Nowadays, most of the designed satellites are dedicated for high performance missions, which require high attitude pointing accuracies. The reaction wheel is the most suitable satellite actuator that can provide high attitude pointing accuracies (0.1°-0.001°). Commonly, three or four reaction wheel...
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| 主要作者: | |
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| 格式: | Thesis |
| 語言: | English |
| 出版: |
2009
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| 主題: | |
| 在線閱讀: | http://psasir.upm.edu.my/id/eprint/51549/1/FK%202009%20119RR.pdf |
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