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

^*此作品的通讯作者

自动化学院

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411 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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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.",

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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.

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Attitude tracking of rigid spacecraft with bounded disturbances

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