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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
2016-07-01
发表期刊PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING
卷号230期号:6页码:498-511
文章类型Article
摘要In 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.
关键词Dual-control Missile Adaptive Sliding Mode Control Robustness Chattering Attenuation
WOS标题词Science & Technology ; Technology
DOI10.1177/0959651816629540
关键词[WOS]ROBUST AUTOPILOT DESIGN ; FLIGHT CONTROL-SYSTEM ; NEURAL-NETWORKS ; DISTURBANCE OBSERVERS ; DYNAMIC INVERSION ; NONLINEAR-SYSTEMS ; GUIDANCE
收录类别SCI
语种英语
项目资助者National Natural Science Foundation of China(61203003 ; 61273149 ; 61273336 ; 61333008)
WOS研究方向Automation & Control Systems
WOS类目Automation & Control Systems
WOS记录号WOS:000378586800002
引用统计
被引频次:2[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/173211/12038
专题综合信息系统研究中心
通讯作者Chang, Yafei
作者单位1.Beijing Inst Control Engn, Beijing 100190, Peoples R China
2.Chinese Acad Sci, Inst Automat, Beijing, Peoples R China
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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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