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	Active fault tolerant control scheme for aircraft with dissimilar redundant actuation system subject to hydraulic failure
	Ijaz, Salman; Yan, Lin; Hamayun, Mirza Tariq; Shi, Cun
刊名	JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS
	2019
卷号	356页码:1302-1332
关键词	Aircraft control Control surfaces Control theory Controllers Fault tolerance Faulting Fighter aircraft Hydraulic actuators Sliding mode control State feedback Active fault tolerant control Electro-hydraulic actuator Fractional-order controllers Integral sliding mode More electric aircraft Recursive least square algorithms Redundant actuation State feedback control law Aircraft hydraulic systems
ISSN号	0016-0032
DOI	10.1016/j.jfranklin.2018.11.018
URL标识	查看原文
收录类别	SCIE ; EI
WOS记录号	WOS:000457636700008
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5922072
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Ijaz, Salman,Yan, Lin,Hamayun, Mirza Tariq,et al. Active fault tolerant control scheme for aircraft with dissimilar redundant actuation system subject to hydraulic failure[J]. JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS,2019,356:1302-1332.
APA	Ijaz, Salman,Yan, Lin,Hamayun, Mirza Tariq,&Shi, Cun.(2019).Active fault tolerant control scheme for aircraft with dissimilar redundant actuation system subject to hydraulic failure.JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS,356,1302-1332.
MLA	Ijaz, Salman,et al."Active fault tolerant control scheme for aircraft with dissimilar redundant actuation system subject to hydraulic failure".JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS 356(2019):1302-1332.

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