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The prescribed time sliding mode control for attitude tracking of spacecraft

Research output: Contribution to Journal/Magazine › Journal article › peer-review

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The prescribed time sliding mode control for attitude tracking of spacecraft. / Chen, Zhirun; Ju, Xiaozhe; Wang, Ziwei et al.
In: Asian Journal of Control, Vol. 24, No. 4, 31.07.2022, p. 1650-1662.

Research output: Contribution to Journal/Magazine › Journal article › peer-review

Harvard

Chen, Z, Ju, X, Wang, Z & Li, Q 2022, 'The prescribed time sliding mode control for attitude tracking of spacecraft', Asian Journal of Control, vol. 24, no. 4, pp. 1650-1662. https://doi.org/10.1002/asjc.2569

APA

Chen, Z., Ju, X., Wang, Z., & Li, Q. (2022). The prescribed time sliding mode control for attitude tracking of spacecraft. Asian Journal of Control, 24(4), 1650-1662. https://doi.org/10.1002/asjc.2569

Vancouver

Chen Z, Ju X, Wang Z, Li Q. The prescribed time sliding mode control for attitude tracking of spacecraft. Asian Journal of Control. 2022 Jul 31;24(4):1650-1662. Epub 2021 May 31. doi: 10.1002/asjc.2569

Author

Chen, Zhirun ; Ju, Xiaozhe ; Wang, Ziwei et al. / The prescribed time sliding mode control for attitude tracking of spacecraft. In: Asian Journal of Control. 2022 ; Vol. 24, No. 4. pp. 1650-1662.

Bibtex

@article{3854ee1671d94a3b940a696be1d48fc4,
title = "The prescribed time sliding mode control for attitude tracking of spacecraft",
abstract = "With the development of the space missions, there are extensive missions in the demand of the prescribed time convergence. However, it's still a difficult work to combine the prescribed time method with the sliding mode control due to the infinite gain of the prescribed time method while approaching the prescribed time and two periods of sliding mode control. In this paper, a new prescribed time sliding mode control method is proposed for general systems with matched disturbances, from the second-order system to the high-order system. A novel sliding mode variable with explicit time term is designed for achieving the prescribed time convergence. More importantly, as time approaches the prescribed time, the singularity of control input can be avoided. Finally, this paper presents a disturbance observer-based prescribed time sliding mode control method for attitude tracking of spacecraft, and the efficiency of this method has been verified through the numerical simulations.",
keywords = "matched disturbances, prescribed time sliding mode control, singularity, spacecraft attitude control",
author = "Zhirun Chen and Xiaozhe Ju and Ziwei Wang and Qing Li",
year = "2022",
month = jul,
day = "31",
doi = "10.1002/asjc.2569",
language = "English",
volume = "24",
pages = "1650--1662",
journal = "Asian Journal of Control",
number = "4",

}

RIS

TY - JOUR

T1 - The prescribed time sliding mode control for attitude tracking of spacecraft

AU - Chen, Zhirun

AU - Ju, Xiaozhe

AU - Wang, Ziwei

AU - Li, Qing

PY - 2022/7/31

Y1 - 2022/7/31

N2 - With the development of the space missions, there are extensive missions in the demand of the prescribed time convergence. However, it's still a difficult work to combine the prescribed time method with the sliding mode control due to the infinite gain of the prescribed time method while approaching the prescribed time and two periods of sliding mode control. In this paper, a new prescribed time sliding mode control method is proposed for general systems with matched disturbances, from the second-order system to the high-order system. A novel sliding mode variable with explicit time term is designed for achieving the prescribed time convergence. More importantly, as time approaches the prescribed time, the singularity of control input can be avoided. Finally, this paper presents a disturbance observer-based prescribed time sliding mode control method for attitude tracking of spacecraft, and the efficiency of this method has been verified through the numerical simulations.

AB - With the development of the space missions, there are extensive missions in the demand of the prescribed time convergence. However, it's still a difficult work to combine the prescribed time method with the sliding mode control due to the infinite gain of the prescribed time method while approaching the prescribed time and two periods of sliding mode control. In this paper, a new prescribed time sliding mode control method is proposed for general systems with matched disturbances, from the second-order system to the high-order system. A novel sliding mode variable with explicit time term is designed for achieving the prescribed time convergence. More importantly, as time approaches the prescribed time, the singularity of control input can be avoided. Finally, this paper presents a disturbance observer-based prescribed time sliding mode control method for attitude tracking of spacecraft, and the efficiency of this method has been verified through the numerical simulations.

KW - matched disturbances

KW - prescribed time sliding mode control

KW - singularity

KW - spacecraft attitude control

U2 - 10.1002/asjc.2569

DO - 10.1002/asjc.2569

M3 - Journal article

VL - 24

SP - 1650

EP - 1662

JO - Asian Journal of Control

JF - Asian Journal of Control

IS - 4

ER -