Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method

Yuhang Wang; Yingmin Jia

doi:10.1007/978-981-16-6320-8_84

Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method

Yuhang Wang
, Yingmin Jia^*

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University

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

Abstract

This brief mainly investigates the fixed-time attitude stabilization problem for flexible spacecraft subject to inertia uncertainties and external disturbances. First of all, based on active disturbance rejection method, extended state observers and gradient projection estimators are combined to estimate the angular velocity and “total disturbance” of spacecraft simultaneously. Then, a saturation-type controller is constructed, which uses terminal sliding mode technique to achieve fixed-time attitude stabilization. Moreover, a sinusoidal compensating term is added in the controller to solve the singularity problem. Finally, numerical simulations are conducted to illustrate the proposed method.

Original language	English
Title of host publication	Proceedings of 2021 Chinese Intelligent Systems Conference
Editors	Yingmin Jia, Weicun Zhang, Yongling Fu, Zhiyuan Yu, Song Zheng
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	813-823
Number of pages	11
ISBN (Print)	9789811663192
DOIs	https://doi.org/10.1007/978-981-16-6320-8_84
State	Published - 2022
Event	17th Chinese Intelligent Systems Conference, CISC 2021 - Fuzhou, China Duration: 16 Oct 2021 → 17 Oct 2021

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	805 LNEE
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	17th Chinese Intelligent Systems Conference, CISC 2021
Country/Territory	China
City	Fuzhou
Period	16/10/21 → 17/10/21

Keywords

Active disturbance rejection method
Fixed-time attitude stabilization
Flexible spacecraft
Terminal sliding mode

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10.1007/978-981-16-6320-8_84

Cite this

Wang, Y., & Jia, Y. (2022). Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method. In Y. Jia, W. Zhang, Y. Fu, Z. Yu, & S. Zheng (Eds.), Proceedings of 2021 Chinese Intelligent Systems Conference (pp. 813-823). (Lecture Notes in Electrical Engineering; Vol. 805 LNEE). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-16-6320-8_84

Wang, Yuhang ; Jia, Yingmin. / Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method. Proceedings of 2021 Chinese Intelligent Systems Conference. editor / Yingmin Jia ; Weicun Zhang ; Yongling Fu ; Zhiyuan Yu ; Song Zheng. Springer Science and Business Media Deutschland GmbH, 2022. pp. 813-823 (Lecture Notes in Electrical Engineering).

@inproceedings{e7660f94ca10493084dadcc70aa6ee2c,

title = "Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method",

abstract = "This brief mainly investigates the fixed-time attitude stabilization problem for flexible spacecraft subject to inertia uncertainties and external disturbances. First of all, based on active disturbance rejection method, extended state observers and gradient projection estimators are combined to estimate the angular velocity and “total disturbance” of spacecraft simultaneously. Then, a saturation-type controller is constructed, which uses terminal sliding mode technique to achieve fixed-time attitude stabilization. Moreover, a sinusoidal compensating term is added in the controller to solve the singularity problem. Finally, numerical simulations are conducted to illustrate the proposed method.",

keywords = "Active disturbance rejection method, Fixed-time attitude stabilization, Flexible spacecraft, Terminal sliding mode",

author = "Yuhang Wang and Yingmin Jia",

note = "Publisher Copyright: {\textcopyright} 2022, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.; 17th Chinese Intelligent Systems Conference, CISC 2021 ; Conference date: 16-10-2021 Through 17-10-2021",

year = "2022",

doi = "10.1007/978-981-16-6320-8\_84",

language = "英语",

isbn = "9789811663192",

series = "Lecture Notes in Electrical Engineering",

publisher = "Springer Science and Business Media Deutschland GmbH",

pages = "813--823",

editor = "Yingmin Jia and Weicun Zhang and Yongling Fu and Zhiyuan Yu and Song Zheng",

booktitle = "Proceedings of 2021 Chinese Intelligent Systems Conference",

address = "德国",

}

Wang, Y & Jia, Y 2022, Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method. in Y Jia, W Zhang, Y Fu, Z Yu & S Zheng (eds), Proceedings of 2021 Chinese Intelligent Systems Conference. Lecture Notes in Electrical Engineering, vol. 805 LNEE, Springer Science and Business Media Deutschland GmbH, pp. 813-823, 17th Chinese Intelligent Systems Conference, CISC 2021, Fuzhou, China, 16/10/21. https://doi.org/10.1007/978-981-16-6320-8_84

Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method. / Wang, Yuhang; Jia, Yingmin.
Proceedings of 2021 Chinese Intelligent Systems Conference. ed. / Yingmin Jia; Weicun Zhang; Yongling Fu; Zhiyuan Yu; Song Zheng. Springer Science and Business Media Deutschland GmbH, 2022. p. 813-823 (Lecture Notes in Electrical Engineering; Vol. 805 LNEE).

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

TY - GEN

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AU - Wang, Yuhang

AU - Jia, Yingmin

PY - 2022

Y1 - 2022

N2 - This brief mainly investigates the fixed-time attitude stabilization problem for flexible spacecraft subject to inertia uncertainties and external disturbances. First of all, based on active disturbance rejection method, extended state observers and gradient projection estimators are combined to estimate the angular velocity and “total disturbance” of spacecraft simultaneously. Then, a saturation-type controller is constructed, which uses terminal sliding mode technique to achieve fixed-time attitude stabilization. Moreover, a sinusoidal compensating term is added in the controller to solve the singularity problem. Finally, numerical simulations are conducted to illustrate the proposed method.

AB - This brief mainly investigates the fixed-time attitude stabilization problem for flexible spacecraft subject to inertia uncertainties and external disturbances. First of all, based on active disturbance rejection method, extended state observers and gradient projection estimators are combined to estimate the angular velocity and “total disturbance” of spacecraft simultaneously. Then, a saturation-type controller is constructed, which uses terminal sliding mode technique to achieve fixed-time attitude stabilization. Moreover, a sinusoidal compensating term is added in the controller to solve the singularity problem. Finally, numerical simulations are conducted to illustrate the proposed method.

KW - Active disturbance rejection method

KW - Fixed-time attitude stabilization

KW - Flexible spacecraft

KW - Terminal sliding mode

UR - https://www.scopus.com/pages/publications/85117913282

U2 - 10.1007/978-981-16-6320-8_84

DO - 10.1007/978-981-16-6320-8_84

M3 - 会议稿件

AN - SCOPUS:85117913282

SN - 9789811663192

T3 - Lecture Notes in Electrical Engineering

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EP - 823

BT - Proceedings of 2021 Chinese Intelligent Systems Conference

A2 - Jia, Yingmin

A2 - Zhang, Weicun

A2 - Fu, Yongling

A2 - Yu, Zhiyuan

A2 - Zheng, Song

PB - Springer Science and Business Media Deutschland GmbH

T2 - 17th Chinese Intelligent Systems Conference, CISC 2021

Y2 - 16 October 2021 through 17 October 2021

ER -

Wang Y, Jia Y. Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method. In Jia Y, Zhang W, Fu Y, Yu Z, Zheng S, editors, Proceedings of 2021 Chinese Intelligent Systems Conference. Springer Science and Business Media Deutschland GmbH. 2022. p. 813-823. (Lecture Notes in Electrical Engineering). doi: 10.1007/978-981-16-6320-8_84

Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method

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Keywords

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