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
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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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