Attitude tracking of rigid spacecraft with bounded disturbances

Yuanqing Xia; Zheng Zhu; Mengyin Fu; Shuo Wang

doi:10.1109/TIE.2010.2046611

Attitude tracking of rigid spacecraft with bounded disturbances

Yuanqing Xia^*, Zheng Zhu, Mengyin Fu, Shuo Wang

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自动化学院

科研成果: 期刊稿件 › 文章 › 同行评审

415 引用（Scopus）

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.

源语言	英语
文章编号	5439851
页（从-至）	647-659
页数	13
期刊	IEEE Transactions on Industrial Electronics
卷	58
期	2
DOI	https://doi.org/10.1109/TIE.2010.2046611
出版状态	已出版 - 2月 2011

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10.1109/TIE.2010.2046611

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Xia, Y., Zhu, Z., Fu, M., & Wang, S. (2011). Attitude tracking of rigid spacecraft with bounded disturbances. IEEE Transactions on Industrial Electronics, 58(2), 647-659. 文章 5439851. https://doi.org/10.1109/TIE.2010.2046611

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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.",

keywords = "Adaptive control, attitude tracking, extended state observer (ESO), sliding-mode control (SMC)",

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AU - Xia, Yuanqing

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AU - Fu, Mengyin

AU - Wang, Shuo

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N2 - 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.

AB - 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.

KW - Adaptive control

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Attitude tracking of rigid spacecraft with bounded disturbances

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