Controller design and stability analysis for spinning missiles via tensor product | |
Zhou, Zhiming; Liu, Zhen![]() ![]() ![]() | |
Source Publication | AEROSPACE SCIENCE AND TECHNOLOGY
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ISSN | 1270-9638 |
2022-11-01 | |
Volume | 130Pages:9 |
Corresponding Author | Liu, Zhen(liuzhen@ia.ac.cn) |
Abstract | 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. |
Keyword | Spinning missile Tensor product model transformation Parallel distributed compensation Model filtering Stability analysis |
DOI | 10.1016/j.ast.2022.107877 |
WOS Keyword | TP-MODEL TRANSFORMATION ; CONING MOTION ; DYNAMIC STABILITY ; INSTABILITY ; AUTOPILOT ; GUIDANCE |
Indexed By | SCI |
Language | 英语 |
Funding Project | 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] |
Funding Organization | National Key Research and Development Program of China ; National Natural Science Foundation of China |
WOS Research Area | Engineering |
WOS Subject | Engineering, Aerospace |
WOS ID | WOS:000860925600001 |
Publisher | ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER |
Citation statistics | |
Document Type | 期刊论文 |
Identifier | http://ir.ia.ac.cn/handle/173211/50315 |
Collection | 综合信息系统研究中心_飞行器智能技术 |
Corresponding Author | Liu, Zhen |
Affiliation | Chinese Acad Sci, Inst Automat, Beijing 100190, Peoples R China |
First Author Affilication | Institute of Automation, Chinese Academy of Sciences |
Corresponding Author Affilication | Institute of Automation, Chinese Academy of Sciences |
Recommended Citation 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. |
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