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Attitude Tracking of Rigid Spacecraft With Bounded Disturbances

文献类型:期刊论文

作者Xia, Yuanqing1; Zhu, Zheng1; Fu, Mengyin1; Wang, Shuo2
刊名IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS
出版日期2011-02-01
卷号58期号:2页码:647-659
关键词Adaptive control attitude tracking extended state observer (ESO) sliding-mode control (SMC)
英文摘要The problem of attitude control for a spacecraft model that is nonlinear in dynamics with inertia uncertainty and external disturbance has been investigated. Adaptive law and extended state observer are applied to estimate the disturbance, by which sliding-mode controllers are designed to combine the two approaches in order to force the state variables of the closed-loop system to converge to the reference attitude states. Also, simulation results are presented to illustrate the effectiveness of the control strategies.
WOS标题词Science & Technology ; Technology
类目[WOS]Automation & Control Systems ; Engineering, Electrical & Electronic ; Instruments & Instrumentation
研究领域[WOS]Automation & Control Systems ; Engineering ; Instruments & Instrumentation
关键词[WOS]QUATERNION FEEDBACK ; REJECTION CONTROL ; ADAPTIVE-CONTROL ; SYSTEMS ; MISSILE ; DELAY
收录类别SCI
语种英语
WOS记录号WOS:000286109500030
源URL[http://ir.ia.ac.cn/handle/173211/3430]  
专题自动化研究所_复杂系统管理与控制国家重点实验室_先进机器人控制团队
作者单位1.Beijing Inst Technol, Dept Automat Control, Beijing 100081, Peoples R China
2.Chinese Acad Sci, Inst Automat, Key Lab Complex Syst & Intelligence Sci, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Xia, Yuanqing,Zhu, Zheng,Fu, Mengyin,et al. Attitude Tracking of Rigid Spacecraft With Bounded Disturbances[J]. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS,2011,58(2):647-659.
APA Xia, Yuanqing,Zhu, Zheng,Fu, Mengyin,&Wang, Shuo.(2011).Attitude Tracking of Rigid Spacecraft With Bounded Disturbances.IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS,58(2),647-659.
MLA Xia, Yuanqing,et al."Attitude Tracking of Rigid Spacecraft With Bounded Disturbances".IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS 58.2(2011):647-659.

入库方式: OAI收割

来源:自动化研究所

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