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

doi:10.1177/0959651816629540

CORC > 自动化研究所 > 中国科学院自动化研究所 > 综合信息系统研究中心

	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
刊名	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
关键词	Dual-control Missile Adaptive Sliding Mode Control Robustness Chattering Attenuation
DOI	10.1177/0959651816629540
文献子类	Article
英文摘要	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.
WOS关键词	ROBUST AUTOPILOT DESIGN ; FLIGHT CONTROL-SYSTEM ; NEURAL-NETWORKS ; DISTURBANCE OBSERVERS ; DYNAMIC INVERSION ; NONLINEAR-SYSTEMS ; GUIDANCE
WOS研究方向	Automation & Control Systems
语种	英语
WOS记录号	WOS:000378586800002
资助机构	National Natural Science Foundation of China(61203003 ; 61273149 ; 61273336 ; 61333008)
内容类型	期刊论文
源URL	[http://ir.ia.ac.cn/handle/173211/12038]
专题	自动化研究所_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
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.