Hybrid Non-Fragile Attitude Stabilization for Post-Capture Spacecraft

Chuang Liu; Ziyu Yang; Xiaokui Yue; Xuechuan Wang

doi:10.1109/CCDC52312.2021.9601750

Hybrid Non-Fragile Attitude Stabilization for Post-Capture Spacecraft

Chuang Liu
, Ziyu Yang
, Xiaokui Yue
, Xuechuan Wang

School of Astronautics

Northwestern Polytechnical University Xian

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

1 Scopus citations

Abstract

This paper investigates the problem of hybrid non-fragile attitude stabilization for post-capture spacecraft in the presence of external disturbances, unknown and uncertain inertia and coexisting controller's gain perturbations. The aim of this work is to design a hybrid non-fragile dynamic output feedback controller such that the closed-loop attitude control system is stabilized, while the actual control input is confined into a certain range. Based on the Lyapunov stability theory, the existence condition of such non-fragile controller is derived in terms of linear matrix inequalities. It is worth mentioning that the controller's additive and multiplicative perturbations are accounted for simultaneously. Finally, an illustrative example is given to demonstrate the effectiveness of the proposed hybrid non-fragile controller.

Original language	English
Title of host publication	Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	6090-6095
Number of pages	6
ISBN (Electronic)	9781665440899
DOIs	https://doi.org/10.1109/CCDC52312.2021.9601750
State	Published - 2021
Event	33rd Chinese Control and Decision Conference, CCDC 2021 - Kunming, China Duration: 22 May 2021 → 24 May 2021

Publication series

Name	Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021

Conference

Conference	33rd Chinese Control and Decision Conference, CCDC 2021
Country/Territory	China
City	Kunming
Period	22/05/21 → 24/05/21

Keywords

Attitude Stabilization
Hybrid Non-fragile Control
Output Feedback Control
Post-capture Spacecraft

Access to Document

10.1109/CCDC52312.2021.9601750

Cite this

Liu, C., Yang, Z., Yue, X., & Wang, X. (2021). Hybrid Non-Fragile Attitude Stabilization for Post-Capture Spacecraft. In Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021 (pp. 6090-6095). (Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC52312.2021.9601750

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title = "Hybrid Non-Fragile Attitude Stabilization for Post-Capture Spacecraft",

abstract = "This paper investigates the problem of hybrid non-fragile attitude stabilization for post-capture spacecraft in the presence of external disturbances, unknown and uncertain inertia and coexisting controller's gain perturbations. The aim of this work is to design a hybrid non-fragile dynamic output feedback controller such that the closed-loop attitude control system is stabilized, while the actual control input is confined into a certain range. Based on the Lyapunov stability theory, the existence condition of such non-fragile controller is derived in terms of linear matrix inequalities. It is worth mentioning that the controller's additive and multiplicative perturbations are accounted for simultaneously. Finally, an illustrative example is given to demonstrate the effectiveness of the proposed hybrid non-fragile controller.",

keywords = "Attitude Stabilization, Hybrid Non-fragile Control, Output Feedback Control, Post-capture Spacecraft",

author = "Chuang Liu and Ziyu Yang and Xiaokui Yue and Xuechuan Wang",

note = "Publisher Copyright: {\textcopyright} 2021 IEEE.; 33rd Chinese Control and Decision Conference, CCDC 2021 ; Conference date: 22-05-2021 Through 24-05-2021",

year = "2021",

doi = "10.1109/CCDC52312.2021.9601750",

language = "英语",

series = "Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021",

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

pages = "6090--6095",

booktitle = "Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021",

}

Liu, C, Yang, Z, Yue, X & Wang, X 2021, Hybrid Non-Fragile Attitude Stabilization for Post-Capture Spacecraft. in Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021. Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021, Institute of Electrical and Electronics Engineers Inc., pp. 6090-6095, 33rd Chinese Control and Decision Conference, CCDC 2021, Kunming, China, 22/05/21. https://doi.org/10.1109/CCDC52312.2021.9601750

Hybrid Non-Fragile Attitude Stabilization for Post-Capture Spacecraft. / Liu, Chuang; Yang, Ziyu; Yue, Xiaokui et al.
Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021. Institute of Electrical and Electronics Engineers Inc., 2021. p. 6090-6095 (Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021).

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

TY - GEN

T1 - Hybrid Non-Fragile Attitude Stabilization for Post-Capture Spacecraft

AU - Liu, Chuang

AU - Yang, Ziyu

AU - Yue, Xiaokui

AU - Wang, Xuechuan

PY - 2021

Y1 - 2021

N2 - This paper investigates the problem of hybrid non-fragile attitude stabilization for post-capture spacecraft in the presence of external disturbances, unknown and uncertain inertia and coexisting controller's gain perturbations. The aim of this work is to design a hybrid non-fragile dynamic output feedback controller such that the closed-loop attitude control system is stabilized, while the actual control input is confined into a certain range. Based on the Lyapunov stability theory, the existence condition of such non-fragile controller is derived in terms of linear matrix inequalities. It is worth mentioning that the controller's additive and multiplicative perturbations are accounted for simultaneously. Finally, an illustrative example is given to demonstrate the effectiveness of the proposed hybrid non-fragile controller.

AB - This paper investigates the problem of hybrid non-fragile attitude stabilization for post-capture spacecraft in the presence of external disturbances, unknown and uncertain inertia and coexisting controller's gain perturbations. The aim of this work is to design a hybrid non-fragile dynamic output feedback controller such that the closed-loop attitude control system is stabilized, while the actual control input is confined into a certain range. Based on the Lyapunov stability theory, the existence condition of such non-fragile controller is derived in terms of linear matrix inequalities. It is worth mentioning that the controller's additive and multiplicative perturbations are accounted for simultaneously. Finally, an illustrative example is given to demonstrate the effectiveness of the proposed hybrid non-fragile controller.

KW - Attitude Stabilization

KW - Hybrid Non-fragile Control

KW - Output Feedback Control

KW - Post-capture Spacecraft

UR - https://www.scopus.com/pages/publications/85125190787

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DO - 10.1109/CCDC52312.2021.9601750

M3 - 会议稿件

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T3 - Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021

SP - 6090

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BT - Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 33rd Chinese Control and Decision Conference, CCDC 2021

Y2 - 22 May 2021 through 24 May 2021

ER -

Hybrid Non-Fragile Attitude Stabilization for Post-Capture Spacecraft

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