A combined attitude and sun tracking system for spacecraft using fuzzy logic control
Many spacecraft attitude control systems today use reaction wheels to deliver precise torques to achieve a three-axis attitude stabilization. Despite the extensive studies in attitude controllers, failures still can occur in a spacecraft system. For example, if a spacec...
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| 格式: | Thesis |
| 语言: | English |
| 出版: |
2019
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| 主题: | |
| 在线阅读: | http://psasir.upm.edu.my/id/eprint/84366/1/FK%202019%20118%20-%20ir.pdf |
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