CASIA OpenIR  > 综合信息系统研究中心  > 飞行器智能技术
Controller design and stability analysis for spinning missiles via tensor product
Zhou, Zhiming; Liu, Zhen; Pan, Yi; Yi, Jianqiang
Source PublicationAEROSPACE SCIENCE AND TECHNOLOGY
ISSN1270-9638
2022-11-01
Volume130Pages:9
Corresponding AuthorLiu, Zhen(liuzhen@ia.ac.cn)
AbstractIn 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.
KeywordSpinning missile Tensor product model transformation Parallel distributed compensation Model filtering Stability analysis
DOI10.1016/j.ast.2022.107877
WOS KeywordTP-MODEL TRANSFORMATION ; CONING MOTION ; DYNAMIC STABILITY ; INSTABILITY ; AUTOPILOT ; GUIDANCE
Indexed BySCI
Language英语
Funding ProjectNational 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 OrganizationNational Key Research and Development Program of China ; National Natural Science Foundation of China
WOS Research AreaEngineering
WOS SubjectEngineering, Aerospace
WOS IDWOS:000860925600001
PublisherELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
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Document Type期刊论文
Identifierhttp://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 AuthorLiu, Zhen
AffiliationChinese Acad Sci, Inst Automat, Beijing 100190, Peoples R China
First Author AffilicationInstitute of Automation, Chinese Academy of Sciences
Corresponding Author AffilicationInstitute 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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