Optimum spacecraft attitude control methods for a combined attitude and thermal control system
Spacecraft missions need efficient and precise attitude control systems. With the aim of reducing the vehicle volume and mass, and for a greater reliability, a system combining the conventional spacecraft attitude control and thermal control systems in a single system is proposed. The combined attit...
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| フォーマット: | 学位論文 |
| 言語: | 英語 |
| 出版事項: |
2011
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| 主題: | |
| オンライン･アクセス: | http://psasir.upm.edu.my/id/eprint/41781/1/FK%202011%206R.pdf |