Full-order sliding mode control for finite-time attitude synchronization of rigid spacecraft with input delay

Yunhan Li; Chunyan Wang; Jianan Wang; Zhou Gu; Jiayuan Shan; Zhuoyue Song

doi:10.1109/CCTA.2019.8920536

Full-order sliding mode control for finite-time attitude synchronization of rigid spacecraft with input delay

Yunhan Li, Chunyan Wang, Jianan Wang, Zhou Gu, Jiayuan Shan, Zhuoyue Song

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

2 Citations (Scopus)

Abstract

This paper investigates finite-time attitude consensus of multi-spacecraft systems with input delay using fullorder sliding mode control. First, the kinematic and dynamic models of spacecraft attitude with disturbance are provided. Then, full-order sliding mode protocol is used to solve the consensus problem. The algorithm is consisted of two layers of sliding mode surfaces, the outer terminal sliding mode manifold and inner fast nonsingular terminal sliding mode manifold. On basis of the control algorithm, this paper considers the input delay of the system, thus a distributed observer is proposed to reduce communication burden and guarantee finite-time convergence, which is proved by Lyapunov stability analysis. Finally, a simulation example is provided to demonstrate the validity the proposed control algorithm.

Original language	English
Title of host publication	CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	166-171
Number of pages	6
ISBN (Electronic)	9781728127675
DOIs	https://doi.org/10.1109/CCTA.2019.8920536
Publication status	Published - Aug 2019
Event	3rd IEEE Conference on Control Technology and Applications, CCTA 2019 - Hong Kong, China Duration: 19 Aug 2019 → 21 Aug 2019

Publication series

Name	CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications

Conference

Conference	3rd IEEE Conference on Control Technology and Applications, CCTA 2019
Country/Territory	China
City	Hong Kong
Period	19/08/19 → 21/08/19

Keywords

Attitude consensus
Finite-time
Full-order sliding mode control
Input delay.

Access to Document

10.1109/CCTA.2019.8920536

Cite this

Li, Y., Wang, C., Wang, J., Gu, Z., Shan, J., & Song, Z. (2019). Full-order sliding mode control for finite-time attitude synchronization of rigid spacecraft with input delay. In CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications (pp. 166-171). Article 8920536 (CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCTA.2019.8920536

Li, Yunhan ; Wang, Chunyan ; Wang, Jianan et al. / Full-order sliding mode control for finite-time attitude synchronization of rigid spacecraft with input delay. CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications. Institute of Electrical and Electronics Engineers Inc., 2019. pp. 166-171 (CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications).

@inproceedings{ededbc191a074cfeb6ccec036e77f559,

title = "Full-order sliding mode control for finite-time attitude synchronization of rigid spacecraft with input delay",

abstract = "This paper investigates finite-time attitude consensus of multi-spacecraft systems with input delay using fullorder sliding mode control. First, the kinematic and dynamic models of spacecraft attitude with disturbance are provided. Then, full-order sliding mode protocol is used to solve the consensus problem. The algorithm is consisted of two layers of sliding mode surfaces, the outer terminal sliding mode manifold and inner fast nonsingular terminal sliding mode manifold. On basis of the control algorithm, this paper considers the input delay of the system, thus a distributed observer is proposed to reduce communication burden and guarantee finite-time convergence, which is proved by Lyapunov stability analysis. Finally, a simulation example is provided to demonstrate the validity the proposed control algorithm.",

keywords = "Attitude consensus, Finite-time, Full-order sliding mode control, Input delay.",

author = "Yunhan Li and Chunyan Wang and Jianan Wang and Zhou Gu and Jiayuan Shan and Zhuoyue Song",

note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 3rd IEEE Conference on Control Technology and Applications, CCTA 2019 ; Conference date: 19-08-2019 Through 21-08-2019",

year = "2019",

month = aug,

doi = "10.1109/CCTA.2019.8920536",

language = "English",

series = "CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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address = "United States",

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Li, Y, Wang, C , Wang, J, Gu, Z, Shan, J & Song, Z 2019, Full-order sliding mode control for finite-time attitude synchronization of rigid spacecraft with input delay. in CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications., 8920536, CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications, Institute of Electrical and Electronics Engineers Inc., pp. 166-171, 3rd IEEE Conference on Control Technology and Applications, CCTA 2019, Hong Kong, China, 19/08/19. https://doi.org/10.1109/CCTA.2019.8920536

Full-order sliding mode control for finite-time attitude synchronization of rigid spacecraft with input delay. / Li, Yunhan; Wang, Chunyan ; Wang, Jianan et al.
CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications. Institute of Electrical and Electronics Engineers Inc., 2019. p. 166-171 8920536 (CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications).

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

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T1 - Full-order sliding mode control for finite-time attitude synchronization of rigid spacecraft with input delay

AU - Li, Yunhan

AU - Wang, Chunyan

AU - Wang, Jianan

AU - Gu, Zhou

AU - Shan, Jiayuan

AU - Song, Zhuoyue

PY - 2019/8

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N2 - This paper investigates finite-time attitude consensus of multi-spacecraft systems with input delay using fullorder sliding mode control. First, the kinematic and dynamic models of spacecraft attitude with disturbance are provided. Then, full-order sliding mode protocol is used to solve the consensus problem. The algorithm is consisted of two layers of sliding mode surfaces, the outer terminal sliding mode manifold and inner fast nonsingular terminal sliding mode manifold. On basis of the control algorithm, this paper considers the input delay of the system, thus a distributed observer is proposed to reduce communication burden and guarantee finite-time convergence, which is proved by Lyapunov stability analysis. Finally, a simulation example is provided to demonstrate the validity the proposed control algorithm.

AB - This paper investigates finite-time attitude consensus of multi-spacecraft systems with input delay using fullorder sliding mode control. First, the kinematic and dynamic models of spacecraft attitude with disturbance are provided. Then, full-order sliding mode protocol is used to solve the consensus problem. The algorithm is consisted of two layers of sliding mode surfaces, the outer terminal sliding mode manifold and inner fast nonsingular terminal sliding mode manifold. On basis of the control algorithm, this paper considers the input delay of the system, thus a distributed observer is proposed to reduce communication burden and guarantee finite-time convergence, which is proved by Lyapunov stability analysis. Finally, a simulation example is provided to demonstrate the validity the proposed control algorithm.

KW - Attitude consensus

KW - Finite-time

KW - Full-order sliding mode control

KW - Input delay.

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BT - CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications

PB - Institute of Electrical and Electronics Engineers Inc.

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Li Y, Wang C , Wang J, Gu Z, Shan J , Song Z. Full-order sliding mode control for finite-time attitude synchronization of rigid spacecraft with input delay. In CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications. Institute of Electrical and Electronics Engineers Inc. 2019. p. 166-171. 8920536. (CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications). doi: 10.1109/CCTA.2019.8920536

Full-order sliding mode control for finite-time attitude synchronization of rigid spacecraft with input delay

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