Fixed-time Attitude Stabilization for Spacecraft Based on Active Disturbance Rejection Method

Yuhang Wang; Yingmin Jia

doi:10.23919/CCC52363.2021.9550742

Fixed-time Attitude Stabilization for Spacecraft Based on Active Disturbance Rejection Method

Yuhang Wang
, Yingmin Jia

School of Automation Science and Electrical Engineering

Beihang University

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

1 Scopus citations

Abstract

This paper mainly investigates the fixed-time attitude stabilization problem of a rigid spacecraft subject to inertia uncertainties and external disturbance. Firstly, a terminal sliding mode surface is constructed to guarantee the fixed time convergence of the attitude independent of initial states. Then, active disturbance rejection control is used to guarantee the states of the spacecraft system reach an arbitrary small vicinity of the terminal sliding mode surface in fixed time. Moreover, to solve the singularity problem in terminal sliding mode control design, an asynchronous switching law is proposed to avoid the singularity. Finally, numerical simulations illustrate the control performance of the proposed control method.

Original language	English
Title of host publication	Proceedings of the 40th Chinese Control Conference, CCC 2021
Editors	Chen Peng, Jian Sun
Publisher	IEEE Computer Society
Pages	7718-7723
Number of pages	6
ISBN (Electronic)	9789881563804
DOIs	https://doi.org/10.23919/CCC52363.2021.9550742
State	Published - 26 Jul 2021
Event	40th Chinese Control Conference, CCC 2021 - Shanghai, China Duration: 26 Jul 2021 → 28 Jul 2021

Publication series

Name	Chinese Control Conference, CCC
Volume	2021-July
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	40th Chinese Control Conference, CCC 2021
Country/Territory	China
City	Shanghai
Period	26/07/21 → 28/07/21

Keywords

Active disturbance rejection control(ADRC)
Fixed-time attitude stabilization
singularity problem
terminal sliding mode(TSM)

Access to Document

10.23919/CCC52363.2021.9550742

Cite this

@inproceedings{3232c69f7cd9403cb0ab8b6d40d3a7dd,

title = "Fixed-time Attitude Stabilization for Spacecraft Based on Active Disturbance Rejection Method",

abstract = "This paper mainly investigates the fixed-time attitude stabilization problem of a rigid spacecraft subject to inertia uncertainties and external disturbance. Firstly, a terminal sliding mode surface is constructed to guarantee the fixed time convergence of the attitude independent of initial states. Then, active disturbance rejection control is used to guarantee the states of the spacecraft system reach an arbitrary small vicinity of the terminal sliding mode surface in fixed time. Moreover, to solve the singularity problem in terminal sliding mode control design, an asynchronous switching law is proposed to avoid the singularity. Finally, numerical simulations illustrate the control performance of the proposed control method.",

keywords = "Active disturbance rejection control(ADRC), Fixed-time attitude stabilization, singularity problem, terminal sliding mode(TSM)",

author = "Yuhang Wang and Yingmin Jia",

note = "Publisher Copyright: {\textcopyright} 2021 Technical Committee on Control Theory, Chinese Association of Automation.; 40th Chinese Control Conference, CCC 2021 ; Conference date: 26-07-2021 Through 28-07-2021",

year = "2021",

month = jul,

day = "26",

doi = "10.23919/CCC52363.2021.9550742",

language = "英语",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "7718--7723",

editor = "Chen Peng and Jian Sun",

booktitle = "Proceedings of the 40th Chinese Control Conference, CCC 2021",

address = "美国",

}

Wang, Y & Jia, Y 2021, Fixed-time Attitude Stabilization for Spacecraft Based on Active Disturbance Rejection Method. in C Peng & J Sun (eds), Proceedings of the 40th Chinese Control Conference, CCC 2021. Chinese Control Conference, CCC, vol. 2021-July, IEEE Computer Society, pp. 7718-7723, 40th Chinese Control Conference, CCC 2021, Shanghai, China, 26/07/21. https://doi.org/10.23919/CCC52363.2021.9550742

Fixed-time Attitude Stabilization for Spacecraft Based on Active Disturbance Rejection Method. / Wang, Yuhang; Jia, Yingmin.
Proceedings of the 40th Chinese Control Conference, CCC 2021. ed. / Chen Peng; Jian Sun. IEEE Computer Society, 2021. p. 7718-7723 (Chinese Control Conference, CCC; Vol. 2021-July).

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

TY - GEN

T1 - Fixed-time Attitude Stabilization for Spacecraft Based on Active Disturbance Rejection Method

AU - Wang, Yuhang

AU - Jia, Yingmin

PY - 2021/7/26

Y1 - 2021/7/26

N2 - This paper mainly investigates the fixed-time attitude stabilization problem of a rigid spacecraft subject to inertia uncertainties and external disturbance. Firstly, a terminal sliding mode surface is constructed to guarantee the fixed time convergence of the attitude independent of initial states. Then, active disturbance rejection control is used to guarantee the states of the spacecraft system reach an arbitrary small vicinity of the terminal sliding mode surface in fixed time. Moreover, to solve the singularity problem in terminal sliding mode control design, an asynchronous switching law is proposed to avoid the singularity. Finally, numerical simulations illustrate the control performance of the proposed control method.

AB - This paper mainly investigates the fixed-time attitude stabilization problem of a rigid spacecraft subject to inertia uncertainties and external disturbance. Firstly, a terminal sliding mode surface is constructed to guarantee the fixed time convergence of the attitude independent of initial states. Then, active disturbance rejection control is used to guarantee the states of the spacecraft system reach an arbitrary small vicinity of the terminal sliding mode surface in fixed time. Moreover, to solve the singularity problem in terminal sliding mode control design, an asynchronous switching law is proposed to avoid the singularity. Finally, numerical simulations illustrate the control performance of the proposed control method.

KW - Active disturbance rejection control(ADRC)

KW - Fixed-time attitude stabilization

KW - singularity problem

KW - terminal sliding mode(TSM)

UR - https://www.scopus.com/pages/publications/85117353847

U2 - 10.23919/CCC52363.2021.9550742

DO - 10.23919/CCC52363.2021.9550742

M3 - 会议稿件

AN - SCOPUS:85117353847

T3 - Chinese Control Conference, CCC

SP - 7718

EP - 7723

BT - Proceedings of the 40th Chinese Control Conference, CCC 2021

A2 - Peng, Chen

A2 - Sun, Jian

PB - IEEE Computer Society

T2 - 40th Chinese Control Conference, CCC 2021

Y2 - 26 July 2021 through 28 July 2021

ER -

Fixed-time Attitude Stabilization for Spacecraft Based on Active Disturbance Rejection Method

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