Enhanced attitude control structure for small satellites with reaction wheels
Attitude accuracies of a three-axis satellite are highly influenced by space environment disturbances and uncertainties. Similar to actuators, an attitude controller also plays an important role and must be robust enough to cope with any disturbances and uncertainties. Various controllers have be...
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| 格式: | Thesis |
| 語言: | 英语 |
| 出版: |
2019
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| 在線閱讀: | http://psasir.upm.edu.my/id/eprint/98227/1/FK%202019%20159%20-%20IR.pdf |