Design of a control moment gyroscope for small satellites

The primary aim of this project is to design a Control Moment Gyroscope (CMG) prototype for single axis control of an agile small satellite. The design should be small, compact and lightweight. Miniature motors and aluminum material were used to reduce the size and weight of the prototype. The overa...

全面介紹

Saved in:
書目詳細資料
主要作者: Tan, Calvin Xian Yang.
其他作者: Low Kay Soon
格式: Final Year Project
語言:English
出版: 2013
主題:
在線閱讀:http://hdl.handle.net/10356/53551
標簽: 添加標簽
沒有標簽, 成為第一個標記此記錄!
機構: Nanyang Technological University
語言: English