H₂ and H ͚ satellite attitude controls for combined energy and attitude control systems

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...

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書目詳細資料
主要作者:	Ban, Ying Siang
格式:	Thesis
語言:	English
出版:	2015
主題:	Artificial satellites - Attitude control systems
在線閱讀:	http://psasir.upm.edu.my/id/eprint/71212/1/FK%202017%2076%20-%20IR.pdf
標簽:	添加標簽沒有標簽, 成為第一個標記此記錄!

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