QQ客服 官方微博 反馈留言

	Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints
	Liu, Zhijie; Liu, Jinkun; Wang, Lijun
刊名	AEROSPACE SCIENCE AND TECHNOLOGY
	2018
卷号	72页码:486-492
关键词	Flexible spacecraft Input magnitude and rate constraints Disturbance observer State feedback control LMI technology
ISSN号	1270-9638
DOI	10.1016/j.ast.2017.11.036
URL标识	查看原文
收录类别	SCIE ; EI
WOS记录号	WOS:000423893800043
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5936117
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Liu, Zhijie,Liu, Jinkun,Wang, Lijun. Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2018,72:486-492.
APA	Liu, Zhijie,Liu, Jinkun,&Wang, Lijun.(2018).Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints.AEROSPACE SCIENCE AND TECHNOLOGY,72,486-492.
MLA	Liu, Zhijie,et al."Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints".AEROSPACE SCIENCE AND TECHNOLOGY 72(2018):486-492.

个性服务

查看访问统计

相关权益政策

暂无数据

收藏/分享

除非特别说明，本系统中所有内容都受版权保护，并保留所有权利。