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	Observer-Based Output Feedback Attitude Stabilization for Spacecraft With Finite-Time Convergence
	Hu, Qinglei; Jiang, Boyan; Zhang, Youmin
刊名	IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY
	2019
卷号	27页码:781-789
关键词	Attitude stabilization finite-time control finite-time observer output feedback
ISSN号	1063-6536
DOI	10.1109/TCST.2017.2780061
URL标识	查看原文
收录类别	SCIE ; EI
WOS记录号	WOS:000457619300026
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5923187
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Hu, Qinglei,Jiang, Boyan,Zhang, Youmin. Observer-Based Output Feedback Attitude Stabilization for Spacecraft With Finite-Time Convergence[J]. IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY,2019,27:781-789.
APA	Hu, Qinglei,Jiang, Boyan,&Zhang, Youmin.(2019).Observer-Based Output Feedback Attitude Stabilization for Spacecraft With Finite-Time Convergence.IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY,27,781-789.
MLA	Hu, Qinglei,et al."Observer-Based Output Feedback Attitude Stabilization for Spacecraft With Finite-Time Convergence".IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY 27(2019):781-789.

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