Attitude maneuvering and vibration damping of flexible spacecraft via robust adaptive backstepping technique

被引：0

作者：

Zhu, Liang-Kuan ^{[1
]}

Ma, Guang-Fu ^{[1
]}

Hu, Qing-Lei ^{[1
]}

机构：

[1] Department of Control Science and Engineering, School of Astronautics, Harbin Institute of Technology, Harbin 150001, China

来源：

Zhendong yu Chongji/Journal of Vibration and Shock | 2009年 / 28卷 / 02期

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：132 / 136

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