Attitude control of missile via fliess expansion

doi:10.1109/TCST.2007.916352

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	Attitude control of missile via fliess expansion
	Yao, Yu 1; Yang, Baoqing 1; He, Fenghua 1; Qiao, Yupeng 2; Cheng, Daizhan2
	2008-09-01
发表期刊	IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY
ISSN	1063-6536
卷号	16 期号:5 页码:959-970
摘要	Motivated by the attitude control of missiles, we consider the tracking problem of nonlinear systems via control with finite admissible values. First, the Fliess functional expansion is used to describe the outputs. Using piecewise admissible value control and the quadratic criteria, the optimal control is obtained. Then for certain model uncertainties, the model predictive control is considered. Online predicted uncertain parameters are used to update the system's dynamics. The method developed is used to the attitude control of missile. Simulation results show the effectiveness of the proposed method.
关键词	attitude control Fliess functional expansion model predictive tracking control nonlinear system
DOI	10.1109/TCST.2007.916352
语种	英语
资助项目	CNSF[60736022] ; CNSF[60674022] ; CNSF[60221301]
WOS研究方向	Automation & Control Systems ; Engineering
WOS类目	Automation & Control Systems ; Engineering, Electrical & Electronic
WOS记录号	WOS:000258822100010
出版者	IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
引用统计
文献类型	期刊论文
条目标识符	http://ir.amss.ac.cn/handle/2S8OKBNM/6917
专题	系统科学研究所
通讯作者	Yao, Yu
作者单位	1.Harbin Inst Technol, Harbin 150080, Peoples R China 2.Acad Sinica, Inst Syst Sci, Beijing 100080, Peoples R China
推荐引用方式 GB/T 7714	Yao, Yu,Yang, Baoqing,He, Fenghua,et al. Attitude control of missile via fliess expansion[J]. IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY,2008,16(5):959-970.
APA	Yao, Yu,Yang, Baoqing,He, Fenghua,Qiao, Yupeng,&Cheng, Daizhan.(2008).Attitude control of missile via fliess expansion.IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY,16(5),959-970.
MLA	Yao, Yu,et al."Attitude control of missile via fliess expansion".IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY 16.5(2008):959-970.