Super-Twisting Disturbance Observer Based Finite-Time Attitude Control for Combined Spacecraft

Wei Zhang; Weijun Yun; Yanning Guo; Yueyong Lv

doi:10.1109/CCDC49329.2020.9164636

Super-Twisting Disturbance Observer Based Finite-Time Attitude Control for Combined Spacecraft

Wei Zhang
, Weijun Yun
, Yanning Guo
, Yueyong Lv

School of Astronautics

Harbin Institute of Technology
Shanghai Minhang District High-Tech Industrialization Promotion Center

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

2 Scopus citations

Abstract

The finite-time attitude control problem for combined spacecraft with non-cooperative target is investigated in this paper. First, a novel dynamic model is developed using the interaction torque between the service and target spacecraft. Next, a super-twisting disturbance observer is improved to estimate the generalized disturbance for the service spacecraft in finite time. Then, a nonlinear terminal sliding mode attitude controller is designed for the combined spacecraft so as to converge the attitude system in finite time. Finally, numerical simulations validate the feasibility of the proposed controller.

Original language	English
Title of host publication	Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	267-271
Number of pages	5
ISBN (Electronic)	9781728158549
DOIs	https://doi.org/10.1109/CCDC49329.2020.9164636
State	Published - Aug 2020
Event	32nd Chinese Control and Decision Conference, CCDC 2020 - Hefei, China Duration: 22 Aug 2020 → 24 Aug 2020

Publication series

Name	Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020

Conference

Conference	32nd Chinese Control and Decision Conference, CCDC 2020
Country/Territory	China
City	Hefei
Period	22/08/20 → 24/08/20

Keywords

Combined spacecraft
Finite-time
Nonsingular terminal sliding mode control
Super-twisting disturbance observer

Access to Document

10.1109/CCDC49329.2020.9164636

Cite this

Zhang, W., Yun, W., Guo, Y., & Lv, Y. (2020). Super-Twisting Disturbance Observer Based Finite-Time Attitude Control for Combined Spacecraft. In Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020 (pp. 267-271). Article 9164636 (Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC49329.2020.9164636

Zhang, Wei ; Yun, Weijun ; Guo, Yanning et al. / Super-Twisting Disturbance Observer Based Finite-Time Attitude Control for Combined Spacecraft. Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020. Institute of Electrical and Electronics Engineers Inc., 2020. pp. 267-271 (Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020).

@inproceedings{0fda267e9d474b5bbfbe51b7fb7ba5a3,

title = "Super-Twisting Disturbance Observer Based Finite-Time Attitude Control for Combined Spacecraft",

abstract = "The finite-time attitude control problem for combined spacecraft with non-cooperative target is investigated in this paper. First, a novel dynamic model is developed using the interaction torque between the service and target spacecraft. Next, a super-twisting disturbance observer is improved to estimate the generalized disturbance for the service spacecraft in finite time. Then, a nonlinear terminal sliding mode attitude controller is designed for the combined spacecraft so as to converge the attitude system in finite time. Finally, numerical simulations validate the feasibility of the proposed controller.",

keywords = "Combined spacecraft, Finite-time, Nonsingular terminal sliding mode control, Super-twisting disturbance observer",

author = "Wei Zhang and Weijun Yun and Yanning Guo and Yueyong Lv",

note = "Publisher Copyright: {\textcopyright} 2020 IEEE.; 32nd Chinese Control and Decision Conference, CCDC 2020 ; Conference date: 22-08-2020 Through 24-08-2020",

year = "2020",

month = aug,

doi = "10.1109/CCDC49329.2020.9164636",

language = "英语",

series = "Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020",

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

pages = "267--271",

booktitle = "Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020",

address = "美国",

}

Zhang, W, Yun, W, Guo, Y & Lv, Y 2020, Super-Twisting Disturbance Observer Based Finite-Time Attitude Control for Combined Spacecraft. in Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020., 9164636, Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020, Institute of Electrical and Electronics Engineers Inc., pp. 267-271, 32nd Chinese Control and Decision Conference, CCDC 2020, Hefei, China, 22/08/20. https://doi.org/10.1109/CCDC49329.2020.9164636

Super-Twisting Disturbance Observer Based Finite-Time Attitude Control for Combined Spacecraft. / Zhang, Wei; Yun, Weijun; Guo, Yanning et al.
Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020. Institute of Electrical and Electronics Engineers Inc., 2020. p. 267-271 9164636 (Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020).

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

TY - GEN

T1 - Super-Twisting Disturbance Observer Based Finite-Time Attitude Control for Combined Spacecraft

AU - Zhang, Wei

AU - Yun, Weijun

AU - Guo, Yanning

AU - Lv, Yueyong

PY - 2020/8

Y1 - 2020/8

N2 - The finite-time attitude control problem for combined spacecraft with non-cooperative target is investigated in this paper. First, a novel dynamic model is developed using the interaction torque between the service and target spacecraft. Next, a super-twisting disturbance observer is improved to estimate the generalized disturbance for the service spacecraft in finite time. Then, a nonlinear terminal sliding mode attitude controller is designed for the combined spacecraft so as to converge the attitude system in finite time. Finally, numerical simulations validate the feasibility of the proposed controller.

AB - The finite-time attitude control problem for combined spacecraft with non-cooperative target is investigated in this paper. First, a novel dynamic model is developed using the interaction torque between the service and target spacecraft. Next, a super-twisting disturbance observer is improved to estimate the generalized disturbance for the service spacecraft in finite time. Then, a nonlinear terminal sliding mode attitude controller is designed for the combined spacecraft so as to converge the attitude system in finite time. Finally, numerical simulations validate the feasibility of the proposed controller.

KW - Combined spacecraft

KW - Finite-time

KW - Nonsingular terminal sliding mode control

KW - Super-twisting disturbance observer

UR - https://www.scopus.com/pages/publications/85091567582

U2 - 10.1109/CCDC49329.2020.9164636

DO - 10.1109/CCDC49329.2020.9164636

M3 - 会议稿件

AN - SCOPUS:85091567582

T3 - Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020

SP - 267

EP - 271

BT - Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 32nd Chinese Control and Decision Conference, CCDC 2020

Y2 - 22 August 2020 through 24 August 2020

ER -

Zhang W, Yun W, Guo Y, Lv Y. Super-Twisting Disturbance Observer Based Finite-Time Attitude Control for Combined Spacecraft. In Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020. Institute of Electrical and Electronics Engineers Inc. 2020. p. 267-271. 9164636. (Proceedings of the 32nd Chinese Control and Decision Conference, CCDC 2020). doi: 10.1109/CCDC49329.2020.9164636

Super-Twisting Disturbance Observer Based Finite-Time Attitude Control for Combined Spacecraft

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this