Designing, Testing and Evaluation of Single Gimbal Control Moment Gyro for Microsatellite
In this paper, a designing procedure of Single Gimbal Control Moment Gyro (SGCMG) for performing an agile slew maneuver in a microsatellite is described, then a prototype is fabricated and finally the test results are presented. The design of actuator mechanism is based on simplicity, direction of p...
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| Автори: | , , , |
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| Формат: | Artigo |
| Мова: | Persa |
| Опубліковано: |
Aerospace Research Institute
2009-03-01
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| Серія: | فصلنامه علوم و فناوری فضایی |
| Предмети: | |
| Онлайн доступ: | https://jsst.ias.ir/article_14373_4661f106f2a787a1aa0dcf7be9382a2d.pdf |
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