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Observer-based adaptive sliding mode control and fuzzy allocation for aero and reaction jets' missile
Chang, Yafei1,2; Yuan, Ruyi2; Tan, Xiangmin2; Yi, Jianqiang2
Source PublicationPROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING
2016-07-01
Volume230Issue:6Pages:498-511
SubtypeArticle
AbstractIn this article, a novel control scheme is proposed to solve the problem of robust and fast tracking control for the longitudinal model of a dual-control missile steered by a combination of aerodynamic fins and reaction jets in the presence of model uncertainties and external disturbances. The control scheme contains two aspects, one is the observer-based adaptive sliding mode control law of the control moment and the other is the fuzzy allocation method which assigns the control moment to the fins and the reaction jets. The main contributions of the article are as follows: (1) to compensate the disturbances and uncertainties on the sliding mode surface and enhance the system robustness, an observer-based sliding mode surface is designed; (2) an adaptive sliding mode control scheme is proposed by introducing an adaptive term derived from radical basis function network, which does not require knowledge of the bound of the system uncertainties and external disturbances. Meanwhile, it eliminates the chattering phenomenon without deteriorating the system fast-response characteristic and robustness; (3) a control-moment allocator based on fuzzy reasoning is designed to make the system respond fast while avoiding wasting of the reaction jets. Simulation results demonstrate that the proposed control scheme is effective in improving control robustness and response rapidity.
KeywordDual-control Missile Adaptive Sliding Mode Control Robustness Chattering Attenuation
WOS HeadingsScience & Technology ; Technology
DOI10.1177/0959651816629540
WOS KeywordROBUST AUTOPILOT DESIGN ; FLIGHT CONTROL-SYSTEM ; NEURAL-NETWORKS ; DISTURBANCE OBSERVERS ; DYNAMIC INVERSION ; NONLINEAR-SYSTEMS ; GUIDANCE
Indexed BySCI
Language英语
Funding OrganizationNational Natural Science Foundation of China(61203003 ; 61273149 ; 61273336 ; 61333008)
WOS Research AreaAutomation & Control Systems
WOS SubjectAutomation & Control Systems
WOS IDWOS:000378586800002
Citation statistics
Cited Times:4[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://ir.ia.ac.cn/handle/173211/12038
Collection综合信息系统研究中心
Corresponding AuthorChang, Yafei
Affiliation1.Beijing Inst Control Engn, Beijing 100190, Peoples R China
2.Chinese Acad Sci, Inst Automat, Beijing, 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
Chang, Yafei,Yuan, Ruyi,Tan, Xiangmin,et al. Observer-based adaptive sliding mode control and fuzzy allocation for aero and reaction jets' missile[J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING,2016,230(6):498-511.
APA Chang, Yafei,Yuan, Ruyi,Tan, Xiangmin,&Yi, Jianqiang.(2016).Observer-based adaptive sliding mode control and fuzzy allocation for aero and reaction jets' missile.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING,230(6),498-511.
MLA Chang, Yafei,et al."Observer-based adaptive sliding mode control and fuzzy allocation for aero and reaction jets' missile".PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING 230.6(2016):498-511.
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