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Attitude Tracking of Rigid Spacecraft With Bounded Disturbances
Xia, Yuanqing1; Zhu, Zheng1; Fu, Mengyin1; Wang, Shuo2
Source PublicationIEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS
2011-02-01
Volume58Issue:2Pages:647-659
SubtypeArticle
Abstract

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.

KeywordAdaptive Control Attitude Tracking Extended State Observer (Eso) Sliding-mode Control (Smc)
WOS HeadingsScience & Technology ; Technology
WOS KeywordQUATERNION FEEDBACK ; REJECTION CONTROL ; ADAPTIVE-CONTROL ; SYSTEMS ; MISSILE ; DELAY
Indexed BySCI
Language英语
WOS Research AreaAutomation & Control Systems ; Engineering ; Instruments & Instrumentation
WOS SubjectAutomation & Control Systems ; Engineering, Electrical & Electronic ; Instruments & Instrumentation
WOS IDWOS:000286109500030
Citation statistics
Cited Times:316[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://ir.ia.ac.cn/handle/173211/3430
Collection复杂系统认知与决策实验室_先进机器人
Affiliation1.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
Recommended Citation
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.
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