Disturbance Observer-Based Adaptive Finite-Time Attitude Tracking Control for Rigid Spacecraft

Jinhui Zhang; Weishuang Zhao; Ganghui Shen; Yuanqing Xia

doi:10.1109/TSMC.2019.2947320

Disturbance Observer-Based Adaptive Finite-Time Attitude Tracking Control for Rigid Spacecraft

Jinhui Zhang^*, Weishuang Zhao, Ganghui Shen, Yuanqing Xia

^*Corresponding author for this work

School of Automation

Beijing Institute of Technology

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

53 Citations (Scopus)

Abstract

This article proposes two kinds of terminal sliding mode control (TSMC) strategies for implementing the finite-time attitude tracking of spacecraft under environmental disturbances and model uncertainties. First, the integral disturbance observer (IDO) is designed to estimate the disturbances and uncertainties. Second, the IDO-based continuous TSMC (CTSMC) method is developed to achieve active disturbance rejection and better tracking performance. Third, to further mitigate the chattering, a modified TSMC (MTSMC) method is constructed by employing an adaptive method and incorporating a piecewise smooth function. Finally, simulations are performed to show the feasibility of the proposed TSMC laws.

Original language	English
Pages (from-to)	6606-6613
Number of pages	8
Journal	IEEE Transactions on Systems, Man, and Cybernetics: Systems
Volume	51
Issue number	11
DOIs	https://doi.org/10.1109/TSMC.2019.2947320
Publication status	Published - 1 Nov 2021

Keywords

Adaptive control
attitude control
finite-time tracking
integral disturbance observer (IDO)
sliding mode control (SMC)

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10.1109/TSMC.2019.2947320

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title = "Disturbance Observer-Based Adaptive Finite-Time Attitude Tracking Control for Rigid Spacecraft",

abstract = "This article proposes two kinds of terminal sliding mode control (TSMC) strategies for implementing the finite-time attitude tracking of spacecraft under environmental disturbances and model uncertainties. First, the integral disturbance observer (IDO) is designed to estimate the disturbances and uncertainties. Second, the IDO-based continuous TSMC (CTSMC) method is developed to achieve active disturbance rejection and better tracking performance. Third, to further mitigate the chattering, a modified TSMC (MTSMC) method is constructed by employing an adaptive method and incorporating a piecewise smooth function. Finally, simulations are performed to show the feasibility of the proposed TSMC laws.",

keywords = "Adaptive control, attitude control, finite-time tracking, integral disturbance observer (IDO), sliding mode control (SMC)",

author = "Jinhui Zhang and Weishuang Zhao and Ganghui Shen and Yuanqing Xia",

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AU - Zhang, Jinhui

AU - Zhao, Weishuang

AU - Shen, Ganghui

AU - Xia, Yuanqing

PY - 2021/11/1

Y1 - 2021/11/1

N2 - This article proposes two kinds of terminal sliding mode control (TSMC) strategies for implementing the finite-time attitude tracking of spacecraft under environmental disturbances and model uncertainties. First, the integral disturbance observer (IDO) is designed to estimate the disturbances and uncertainties. Second, the IDO-based continuous TSMC (CTSMC) method is developed to achieve active disturbance rejection and better tracking performance. Third, to further mitigate the chattering, a modified TSMC (MTSMC) method is constructed by employing an adaptive method and incorporating a piecewise smooth function. Finally, simulations are performed to show the feasibility of the proposed TSMC laws.

AB - This article proposes two kinds of terminal sliding mode control (TSMC) strategies for implementing the finite-time attitude tracking of spacecraft under environmental disturbances and model uncertainties. First, the integral disturbance observer (IDO) is designed to estimate the disturbances and uncertainties. Second, the IDO-based continuous TSMC (CTSMC) method is developed to achieve active disturbance rejection and better tracking performance. Third, to further mitigate the chattering, a modified TSMC (MTSMC) method is constructed by employing an adaptive method and incorporating a piecewise smooth function. Finally, simulations are performed to show the feasibility of the proposed TSMC laws.

KW - Adaptive control

KW - attitude control

KW - finite-time tracking

KW - integral disturbance observer (IDO)

KW - sliding mode control (SMC)

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SN - 2168-2216

VL - 51

SP - 6606

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JO - IEEE Transactions on Systems, Man, and Cybernetics: Systems

JF - IEEE Transactions on Systems, Man, and Cybernetics: Systems

IS - 11

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Disturbance Observer-Based Adaptive Finite-Time Attitude Tracking Control for Rigid Spacecraft

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Keywords

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