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Controller design and stability analysis for spinning missiles via tensor product

文献类型：期刊论文

作者Zhou, Zhiming; Liu, Zhen; Pan, Yi; Yi, Jianqiang
刊名AEROSPACE SCIENCE AND TECHNOLOGY
出版日期2022-11-01
卷号130页码:9
关键词Spinning missile Tensor product model transformation Parallel distributed compensation Model filtering Stability analysis
ISSN号1270-9638
DOI10.1016/j.ast.2022.107877
通讯作者Liu, Zhen(liuzhen@ia.ac.cn)
英文摘要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.
WOS关键词TP-MODEL TRANSFORMATION ; CONING MOTION ; DYNAMIC STABILITY ; INSTABILITY ; AUTOPILOT ; GUIDANCE
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]
WOS研究方向Engineering
语种英语
WOS记录号WOS:000860925600001
出版者ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
资助机构National Key Research and Development Program of China ; National Natural Science Foundation of China
源URL[http://ir.ia.ac.cn/handle/173211/50314]  
专题综合信息系统研究中心_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
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.

入库方式： OAI收割

来源：自动化研究所

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