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Attitude control of missile via fliess expansion

文献类型：期刊论文

作者Yao, Yu1; Yang, Baoqing1; He, Fenghua1; Qiao, Yupeng2; Cheng, Daizhan2
刊名IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY
出版日期2008-09-01
卷号16期号:5页码:959-970
关键词attitude control Fliess functional expansion model predictive tracking control nonlinear system
ISSN号1063-6536
DOI10.1109/TCST.2007.916352
英文摘要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.
资助项目CNSF[60736022] ; CNSF[60674022] ; CNSF[60221301]
WOS研究方向Automation & Control Systems ; Engineering
语种英语
WOS记录号WOS:000258822100010
出版者IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
源URL[http://ir.amss.ac.cn/handle/2S8OKBNM/6916]  
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.

入库方式： OAI收割

来源：数学与系统科学研究院

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