Controller design and stability analysis for spinning missiles via tensor product

doi:10.1016/j.ast.2022.107877

	Controller design and stability analysis for spinning missiles via tensor product
	Zhou, Zhiming; Liu, Zhen; Pan, Yi; Yi, Jianqiang
发表期刊	AEROSPACE SCIENCE AND TECHNOLOGY
ISSN	1270-9638
	2022-11-01
卷号	130 页码:9
通讯作者	Liu, Zhen(liuzhen@ia.ac.cn)
摘要	In this paper, the controller design and stability analysis for the parameters time-varying model of spinning missiles are investigated. A mathematical model for the spinning missile considering the flight parameters varying with time is proposed. Based on tensor product (TP) model transformation for the spinning missile, the parallel distributed compensation (PDC) state feedback controller is designed, and the stability of the controlled system is analyzed with the tool of linear matrix inequalities (LMIs). Numerical simulations with time-varying parameters are conducted to demonstrate the effectiveness of the proposed controller. The given controller can not only guarantee the steady performance but also the decoupling performance between pitch and yaw channels when used in the flight parameters time -varying spinning missiles.(c) 2022 Elsevier Masson SAS. All rights reserved.
关键词	Spinning missile Tensor product model transformation Parallel distributed compensation Model filtering Stability analysis
DOI	10.1016/j.ast.2022.107877
关键词[WOS]	TP-MODEL TRANSFORMATION ; CONING MOTION ; DYNAMIC STABILITY ; INSTABILITY ; AUTOPILOT ; GUIDANCE
收录类别	SCI
语种	英语
资助项目	National Key Research and Development Program of China[2018AAA0102402] ; National Natural Science Foundation of China[61906197] ; National Natural Science Foundation of China[2019- JCJQ-ZD-049]
项目资助者	National Key Research and Development Program of China ; National Natural Science Foundation of China
WOS研究方向	Engineering
WOS类目	Engineering, Aerospace
WOS记录号	WOS:000860925600001
出版者	ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
引用统计	被引频次：1[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://ir.ia.ac.cn/handle/173211/50315
专题	复杂系统认知与决策实验室_飞行器智能技术
通讯作者	Liu, Zhen
作者单位	Chinese Acad Sci, Inst Automat, Beijing 100190, Peoples R China
第一作者单位	中国科学院自动化研究所
通讯作者单位	中国科学院自动化研究所
推荐引用方式 GB/T 7714	Zhou, Zhiming,Liu, Zhen,Pan, Yi,et al. Controller design and stability analysis for spinning missiles via tensor product[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2022,130:9.
APA	Zhou, Zhiming,Liu, Zhen,Pan, Yi,&Yi, Jianqiang.(2022).Controller design and stability analysis for spinning missiles via tensor product.AEROSPACE SCIENCE AND TECHNOLOGY,130,9.
MLA	Zhou, Zhiming,et al."Controller design and stability analysis for spinning missiles via tensor product".AEROSPACE SCIENCE AND TECHNOLOGY 130(2022):9.