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

^*Corresponding author for this work

School of Automation

Research output: Contribution to journal › Article › peer-review

411 Citations (Scopus)

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.

Original language	English
Article number	5439851
Pages (from-to)	647-659
Number of pages	13
Journal	IEEE Transactions on Industrial Electronics
Volume	58
Issue number	2
DOIs	https://doi.org/10.1109/TIE.2010.2046611
Publication status	Published - Feb 2011

Keywords

Adaptive control
attitude tracking
extended state observer (ESO)
sliding-mode control (SMC)

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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.",

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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.

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KW - Adaptive control

KW - attitude tracking

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KW - sliding-mode control (SMC)

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Attitude tracking of rigid spacecraft with bounded disturbances

Abstract

Keywords

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