Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode

Chao Gan; Pingli Lu; Xiangdong Liu; Dapeng Yang

doi:10.1109/WCICA.2014.7053150

Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode

Chao Gan, Pingli Lu, Xiangdong Liu, Dapeng Yang

School of Automation

Beijing Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Citations (Scopus)

Abstract

In this paper, the distributed cooperative attitude tracking control law based on a new modified fast terminal sliding mode is presented for multiple spacecraft formation flying in the presence of model uncertainty and external disturbance. Firstly, to speed the convergence rate and avoid the singularity problem, a new modified fast terminal sliding mode manifold is proposed. Then, based on the proposed terminal sliding mode manifold, the distributed cooperative attitude tracking controller is designed for the spacecraft formation flying(SFF) in the presence of model uncertainty and external disturbance, Meanwhile, the finite time stability of SFF system can be also guaranteed. Finally, numerical simulation is given to verify the validity of the proposed control algorithm.

Original language	English
Title of host publication	Proceeding of the 11th World Congress on Intelligent Control and Automation, WCICA 2014
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	2687-2692
Number of pages	6
Edition	March
ISBN (Electronic)	9781479958252
DOIs	https://doi.org/10.1109/WCICA.2014.7053150
Publication status	Published - 2 Mar 2015
Event	2014 11th World Congress on Intelligent Control and Automation, WCICA 2014 - Shenyang, China Duration: 29 Jun 2014 → 4 Jul 2014

Publication series

Name	Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
Number	March
Volume	2015-March

Conference

Conference	2014 11th World Congress on Intelligent Control and Automation, WCICA 2014
Country/Territory	China
City	Shenyang
Period	29/06/14 → 4/07/14

Keywords

Attitude tracking
Spacecraft formation flying
Terminal sliding mode

Access to Document

10.1109/WCICA.2014.7053150

Cite this

Gan, C., Lu, P., Liu, X., & Yang, D. (2015). Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode. In Proceeding of the 11th World Congress on Intelligent Control and Automation, WCICA 2014 (March ed., pp. 2687-2692). Article 7053150 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA); Vol. 2015-March, No. March). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/WCICA.2014.7053150

Gan, Chao ; Lu, Pingli ; Liu, Xiangdong et al. / Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode. Proceeding of the 11th World Congress on Intelligent Control and Automation, WCICA 2014. March. ed. Institute of Electrical and Electronics Engineers Inc., 2015. pp. 2687-2692 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA); March).

@inproceedings{0dca165508c04005adef3da268c0159f,

title = "Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode",

abstract = "In this paper, the distributed cooperative attitude tracking control law based on a new modified fast terminal sliding mode is presented for multiple spacecraft formation flying in the presence of model uncertainty and external disturbance. Firstly, to speed the convergence rate and avoid the singularity problem, a new modified fast terminal sliding mode manifold is proposed. Then, based on the proposed terminal sliding mode manifold, the distributed cooperative attitude tracking controller is designed for the spacecraft formation flying(SFF) in the presence of model uncertainty and external disturbance, Meanwhile, the finite time stability of SFF system can be also guaranteed. Finally, numerical simulation is given to verify the validity of the proposed control algorithm.",

keywords = "Attitude tracking, Spacecraft formation flying, Terminal sliding mode",

author = "Chao Gan and Pingli Lu and Xiangdong Liu and Dapeng Yang",

note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; 2014 11th World Congress on Intelligent Control and Automation, WCICA 2014 ; Conference date: 29-06-2014 Through 04-07-2014",

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series = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",

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Gan, C, Lu, P , Liu, X & Yang, D 2015, Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode. in Proceeding of the 11th World Congress on Intelligent Control and Automation, WCICA 2014. March edn, 7053150, Proceedings of the World Congress on Intelligent Control and Automation (WCICA), no. March, vol. 2015-March, Institute of Electrical and Electronics Engineers Inc., pp. 2687-2692, 2014 11th World Congress on Intelligent Control and Automation, WCICA 2014, Shenyang, China, 29/06/14. https://doi.org/10.1109/WCICA.2014.7053150

Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode. / Gan, Chao; Lu, Pingli ; Liu, Xiangdong et al.
Proceeding of the 11th World Congress on Intelligent Control and Automation, WCICA 2014. March. ed. Institute of Electrical and Electronics Engineers Inc., 2015. p. 2687-2692 7053150 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA); Vol. 2015-March, No. March).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode

AU - Gan, Chao

AU - Lu, Pingli

AU - Liu, Xiangdong

AU - Yang, Dapeng

PY - 2015/3/2

Y1 - 2015/3/2

N2 - In this paper, the distributed cooperative attitude tracking control law based on a new modified fast terminal sliding mode is presented for multiple spacecraft formation flying in the presence of model uncertainty and external disturbance. Firstly, to speed the convergence rate and avoid the singularity problem, a new modified fast terminal sliding mode manifold is proposed. Then, based on the proposed terminal sliding mode manifold, the distributed cooperative attitude tracking controller is designed for the spacecraft formation flying(SFF) in the presence of model uncertainty and external disturbance, Meanwhile, the finite time stability of SFF system can be also guaranteed. Finally, numerical simulation is given to verify the validity of the proposed control algorithm.

AB - In this paper, the distributed cooperative attitude tracking control law based on a new modified fast terminal sliding mode is presented for multiple spacecraft formation flying in the presence of model uncertainty and external disturbance. Firstly, to speed the convergence rate and avoid the singularity problem, a new modified fast terminal sliding mode manifold is proposed. Then, based on the proposed terminal sliding mode manifold, the distributed cooperative attitude tracking controller is designed for the spacecraft formation flying(SFF) in the presence of model uncertainty and external disturbance, Meanwhile, the finite time stability of SFF system can be also guaranteed. Finally, numerical simulation is given to verify the validity of the proposed control algorithm.

KW - Attitude tracking

KW - Spacecraft formation flying

KW - Terminal sliding mode

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M3 - Conference contribution

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T3 - Proceedings of the World Congress on Intelligent Control and Automation (WCICA)

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BT - Proceeding of the 11th World Congress on Intelligent Control and Automation, WCICA 2014

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Gan C, Lu P , Liu X, Yang D. Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode. In Proceeding of the 11th World Congress on Intelligent Control and Automation, WCICA 2014. March ed. Institute of Electrical and Electronics Engineers Inc. 2015. p. 2687-2692. 7053150. (Proceedings of the World Congress on Intelligent Control and Automation (WCICA); March). doi: 10.1109/WCICA.2014.7053150

Distributed cooperative attitude tracking control for multiple rigid spacecraft using fast terminal sliding mode

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