中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Finite-time attitude tracking control for spacecraft with uncertain actuator configuration

文献类型:期刊论文

作者Hu QL(胡庆雷); Yu, Yanbo; Li B(李波); Qi JT(齐俊桐)
刊名Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
出版日期2015
卷号229期号:13页码:2457-2468
关键词Spacecraft finite-time contro l backstepping terminal sliding mode actuator configuration
ISSN号0954-4100
产权排序1
通讯作者胡庆雷
中文摘要The issue of attitude tracking control with finite-time convergence is investigated for spacecraft in the presence of external disturbance and uncertain actuator configuration as well. More specifically, in view of backstepping technique, the attitude quaternion can firstly track the demanded command in finite time under the virtual control law by introducing a novel terminal sliding manifold. Then, the finite-time convergence to the sliding mode of the angular velocity error will be achieved under the proposed novel finite-time control and a parameter updating law, even under uncertain actuator misalignment. In addition, the finite-time stabilization/convergence of the sliding surface and the spacecraft attitude tracking error have been proved and analyzed using the Lyapunov method theoretically. Finally, numerical simulation results are presented to illustrate the performance of the proposed scheme. © IMechE 2015.
WOS标题词Science & Technology ; Technology
类目[WOS]Engineering, Aerospace ; Engineering, Mechanical
研究领域[WOS]Engineering
关键词[WOS]TERMINAL SLIDING MODE ; RIGID SPACECRAFT ; CONTROL DESIGN ; STABILIZATION ; MISALIGNMENT ; CONVERGENCE ; CONSTRAINTS ; MANEUVERS ; SYSTEMS
收录类别SCI ; EI
语种英语
WOS记录号WOS:000363206800009
源URL[http://ir.sia.cn/handle/173321/17141]  
专题沈阳自动化研究所_机器人学研究室
推荐引用方式
GB/T 7714
Hu QL,Yu, Yanbo,Li B,et al. Finite-time attitude tracking control for spacecraft with uncertain actuator configuration[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2015,229(13):2457-2468.
APA Hu QL,Yu, Yanbo,Li B,&Qi JT.(2015).Finite-time attitude tracking control for spacecraft with uncertain actuator configuration.Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,229(13),2457-2468.
MLA Hu QL,et al."Finite-time attitude tracking control for spacecraft with uncertain actuator configuration".Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 229.13(2015):2457-2468.

入库方式: OAI收割

来源:沈阳自动化研究所

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