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^*

^*此作品的通讯作者

自动化科学与电气工程学院

Beihang University

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

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.

源语言	英语
主期刊名	Proceedings of 2021 Chinese Intelligent Systems Conference
编辑	Yingmin Jia, Weicun Zhang, Yongling Fu, Zhiyuan Yu, Song Zheng
出版商	Springer Science and Business Media Deutschland GmbH
页	813-823
页数	11
ISBN（印刷版）	9789811663192
DOI	https://doi.org/10.1007/978-981-16-6320-8_84
出版状态	已出版 - 2022
活动	17th Chinese Intelligent Systems Conference, CISC 2021 - Fuzhou, 中国期限: 16 10月 2021 → 17 10月 2021

出版系列

姓名	Lecture Notes in Electrical Engineering
卷	805 LNEE
ISSN（印刷版）	1876-1100
ISSN（电子版）	1876-1119

会议

会议	17th Chinese Intelligent Systems Conference, CISC 2021
国家/地区	中国
市	Fuzhou
时期	16/10/21 → 17/10/21

访问文件

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

其它文件与链接

链接到 Scopus 的出版物

引用此

Wang, Y., & Jia, Y. (2022). Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method. 在 Y. Jia, W. Zhang, Y. Fu, Z. Yu, & S. Zheng (编辑), Proceedings of 2021 Chinese Intelligent Systems Conference (页码 813-823). (Lecture Notes in Electrical Engineering; 卷 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. 编辑 / Yingmin Jia ; Weicun Zhang ; Yongling Fu ; Zhiyuan Yu ; Song Zheng. Springer Science and Business Media Deutschland GmbH, 2022. 页码 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. 在 Y Jia, W Zhang, Y Fu, Z Yu & S Zheng (编辑), Proceedings of 2021 Chinese Intelligent Systems Conference. Lecture Notes in Electrical Engineering, 卷 805 LNEE, Springer Science and Business Media Deutschland GmbH, 页码 813-823, 17th Chinese Intelligent Systems Conference, CISC 2021, Fuzhou, 中国, 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. 编辑 / Yingmin Jia; Weicun Zhang; Yongling Fu; Zhiyuan Yu; Song Zheng. Springer Science and Business Media Deutschland GmbH, 2022. 页码 813-823 (Lecture Notes in Electrical Engineering; 卷 805 LNEE).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - Robust Fixed-Time Attitude Stabilization of Flexible Spacecraft via Active Disturbance Rejection Method

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

SP - 813

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. 在 Jia Y, Zhang W, Fu Y, Yu Z, Zheng S, 编辑, Proceedings of 2021 Chinese Intelligent Systems Conference. Springer Science and Business Media Deutschland GmbH. 2022. 页码 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

摘要

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会议

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