Sliding mode control techniques for combined energy and attitude control system
Attitude control and power storage subsystems are two of the essential utilities provided on a satellite. As they compromise a significant fraction of a satellite’s weight, a synergism concept that integrates these two into one subsystem can reduce the mass and volume of a satellite. The reduction w...
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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/67704/1/FK%202015%20111%20IR.pdf |