H₂ and H ͚ satellite attitude controls for combined energy and attitude control systems
Combined Energy Storage and Attitude Control System (CEACS) is a new satellite system developed using flywheels to offer mass reduction, longer operation life and also cost reduction. To date, the demonstration of the CEACS attitude control performance has been limited only to the proportional de...
| 第一著者: | |
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| フォーマット: | 学位論文 |
| 言語: | 英語 |
| 出版事項: |
2015
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| 主題: | |
| オンライン･アクセス: | http://psasir.upm.edu.my/id/eprint/71212/1/FK%202017%2076%20-%20IR%281%29edited.pdf |