Observer-based adaptive sliding mode control and fuzzy allocation for aero and reaction jets' missile

doi:10.1177/0959651816629540

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	Observer-based adaptive sliding mode control and fuzzy allocation for aero and reaction jets' missile
	Chang, Yafei 1,2; Yuan, Ruyi2 ; Tan, Xiangmin2 ; Yi, Jianqiang2
发表期刊	PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING
	2016-07-01
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
DOI	10.1177/0959651816629540
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：7[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
第一作者单位	中国科学院自动化研究所
通讯作者单位	中国科学院自动化研究所
推荐引用方式 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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