Fixed-time nonsingular terminal sliding mode control for spacecraft rendezvous

Jingwei Dong; Chuanjiang Li; Boyan Jiang; Yanchao Sun

doi:10.1109/CCDC.2017.7979446

Fixed-time nonsingular terminal sliding mode control for spacecraft rendezvous

Jingwei Dong
, Chuanjiang Li
, Boyan Jiang
, Yanchao Sun

School of Astronautics

Harbin Institute of Technology

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

6 Scopus citations

Abstract

This paper presents a fixed-time nonsingular terminal sliding mode control methodology for spacecraft rendezvous in the presence of nonlinearity and external disturbance. A nonsingular terminal sliding surface is constructed and a continuous sinusoidal function is introduced into the controller to solve the inherent singularity problem. Under the proposed controller, the relative position of the chaser spacecraft can rendezvous with the target within fixed time, which is demonstrated by Lyapunov theorem. The simulation results show that the proposed controller enables rapid convergence rate, high precision and strong robustness in the presence of nonlinearity and external disturbance.

Original language	English
Title of host publication	Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	5340-5345
Number of pages	6
ISBN (Electronic)	9781509046560
DOIs	https://doi.org/10.1109/CCDC.2017.7979446
State	Published - 12 Jul 2017
Event	29th Chinese Control and Decision Conference, CCDC 2017 - Chongqing, China Duration: 28 May 2017 → 30 May 2017

Publication series

Name	Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

Conference

Conference	29th Chinese Control and Decision Conference, CCDC 2017
Country/Territory	China
City	Chongqing
Period	28/05/17 → 30/05/17

Keywords

Elliptical orbit
Fixed-time stability
Nonsingular terminal sliding mode
Relative position control
Spacecraft rendezvous

Access to Document

10.1109/CCDC.2017.7979446

Cite this

Dong, J., Li, C., Jiang, B., & Sun, Y. (2017). Fixed-time nonsingular terminal sliding mode control for spacecraft rendezvous. In Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017 (pp. 5340-5345). Article 7979446 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC.2017.7979446

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title = "Fixed-time nonsingular terminal sliding mode control for spacecraft rendezvous",

abstract = "This paper presents a fixed-time nonsingular terminal sliding mode control methodology for spacecraft rendezvous in the presence of nonlinearity and external disturbance. A nonsingular terminal sliding surface is constructed and a continuous sinusoidal function is introduced into the controller to solve the inherent singularity problem. Under the proposed controller, the relative position of the chaser spacecraft can rendezvous with the target within fixed time, which is demonstrated by Lyapunov theorem. The simulation results show that the proposed controller enables rapid convergence rate, high precision and strong robustness in the presence of nonlinearity and external disturbance.",

keywords = "Elliptical orbit, Fixed-time stability, Nonsingular terminal sliding mode, Relative position control, Spacecraft rendezvous",

author = "Jingwei Dong and Chuanjiang Li and Boyan Jiang and Yanchao Sun",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 29th Chinese Control and Decision Conference, CCDC 2017 ; Conference date: 28-05-2017 Through 30-05-2017",

year = "2017",

month = jul,

day = "12",

doi = "10.1109/CCDC.2017.7979446",

language = "英语",

series = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",

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

pages = "5340--5345",

booktitle = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",

address = "美国",

}

Dong, J, Li, C, Jiang, B & Sun, Y 2017, Fixed-time nonsingular terminal sliding mode control for spacecraft rendezvous. in Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017., 7979446, Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017, Institute of Electrical and Electronics Engineers Inc., pp. 5340-5345, 29th Chinese Control and Decision Conference, CCDC 2017, Chongqing, China, 28/05/17. https://doi.org/10.1109/CCDC.2017.7979446

Fixed-time nonsingular terminal sliding mode control for spacecraft rendezvous. / Dong, Jingwei; Li, Chuanjiang; Jiang, Boyan et al.
Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc., 2017. p. 5340-5345 7979446 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017).

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

TY - GEN

T1 - Fixed-time nonsingular terminal sliding mode control for spacecraft rendezvous

AU - Dong, Jingwei

AU - Li, Chuanjiang

AU - Jiang, Boyan

AU - Sun, Yanchao

PY - 2017/7/12

Y1 - 2017/7/12

N2 - This paper presents a fixed-time nonsingular terminal sliding mode control methodology for spacecraft rendezvous in the presence of nonlinearity and external disturbance. A nonsingular terminal sliding surface is constructed and a continuous sinusoidal function is introduced into the controller to solve the inherent singularity problem. Under the proposed controller, the relative position of the chaser spacecraft can rendezvous with the target within fixed time, which is demonstrated by Lyapunov theorem. The simulation results show that the proposed controller enables rapid convergence rate, high precision and strong robustness in the presence of nonlinearity and external disturbance.

AB - This paper presents a fixed-time nonsingular terminal sliding mode control methodology for spacecraft rendezvous in the presence of nonlinearity and external disturbance. A nonsingular terminal sliding surface is constructed and a continuous sinusoidal function is introduced into the controller to solve the inherent singularity problem. Under the proposed controller, the relative position of the chaser spacecraft can rendezvous with the target within fixed time, which is demonstrated by Lyapunov theorem. The simulation results show that the proposed controller enables rapid convergence rate, high precision and strong robustness in the presence of nonlinearity and external disturbance.

KW - Elliptical orbit

KW - Fixed-time stability

KW - Nonsingular terminal sliding mode

KW - Relative position control

KW - Spacecraft rendezvous

UR - https://www.scopus.com/pages/publications/85028054819

U2 - 10.1109/CCDC.2017.7979446

DO - 10.1109/CCDC.2017.7979446

M3 - 会议稿件

AN - SCOPUS:85028054819

T3 - Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

SP - 5340

EP - 5345

BT - Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 29th Chinese Control and Decision Conference, CCDC 2017

Y2 - 28 May 2017 through 30 May 2017

ER -

Dong J, Li C, Jiang B, Sun Y. Fixed-time nonsingular terminal sliding mode control for spacecraft rendezvous. In Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 5340-5345. 7979446. (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017). doi: 10.1109/CCDC.2017.7979446

Fixed-time nonsingular terminal sliding mode control for spacecraft rendezvous

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