Attitude control and vibration suppression for flexible spacecraft using control moment gyroscopes

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作者：
机构：
[1] Hu, Quan
[2] Zhang, Jingrui
来源：
Hu, Quan (huquan2690@hotmail.com) | 1600年 / American Society of Civil Engineers (ASCE), United States卷 / 29期
基金：
中国国家自然科学基金;
关键词：
Flexible spacecraft - Equations of motion - Numerical methods - Stabilization - Controllers - Gyroscopes;
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