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	Adaptive integrated guidance and control backstepping sliding mode design for blended control missile [复合控制导弹反步滑模IGC自适应设计方法]
	Xia, C.; Dong, C.; Wang, Q.; Cheng, H.
刊名	Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics
	2018
卷号	40页码:2325-2333
关键词	Backstepping Design Electronic guidance systems Error compensation Guided missiles Integer programming Sliding mode control State estimation Adaptive compensation Adaptive Control Extended state observer Integrated guidance and control (IGC) Terminal sliding mode Virtual control Adaptive control systems
ISSN号	1001506X
DOI	10.3969/j.issn.1001-506X.2018.10.25
URL标识	查看原文
收录类别	EI ; CSCD
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5928981
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Xia, C.,Dong, C.,Wang, Q.,等. Adaptive integrated guidance and control backstepping sliding mode design for blended control missile [复合控制导弹反步滑模IGC自适应设计方法][J]. Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics,2018,40:2325-2333.
APA	Xia, C.,Dong, C.,Wang, Q.,&Cheng, H..(2018).Adaptive integrated guidance and control backstepping sliding mode design for blended control missile [复合控制导弹反步滑模IGC自适应设计方法].Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics,40,2325-2333.
MLA	Xia, C.,et al."Adaptive integrated guidance and control backstepping sliding mode design for blended control missile [复合控制导弹反步滑模IGC自适应设计方法]".Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics 40(2018):2325-2333.

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