Spacecraft Attitude Tracking Control Based on High-Order Fully Actuated System Approach

Dongyan Jin; Shixiang Jia; Tong Wang; Jianbin Qiu

doi:10.1109/CFASTA57821.2023.10243176

Spacecraft Attitude Tracking Control Based on High-Order Fully Actuated System Approach

Dongyan Jin^*
, Shixiang Jia
, Tong Wang
, Jianbin Qiu

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

5 Scopus citations

Abstract

This paper focuses on the attitude tracking control of spacecraft. Firstly, the modified Rodrigues parameters are selected to characterize the spacecraft's attitude, whose mathematical model is then established by considering the uncertainties of the spacecraft parameters and the bounded disturbances. The mathematical model of the spacecraft is transformed into a type of high-order fully actuated (HOFA) system with uncertainties. Then, based on the HOFA system approach, a robust controller for a type of HOFA system with uncertainties is designed, which can ensure that the system states converge to an arbitrary ellipsoidal region. Finally, the validness of the designed controller is verified by simulation.

Original language	English
Title of host publication	Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1040-1044
Number of pages	5
ISBN (Electronic)	9798350332162
DOIs	https://doi.org/10.1109/CFASTA57821.2023.10243176
State	Published - 2023
Event	2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023 - Qingdao, China Duration: 14 Jul 2023 → 16 Jul 2023

Publication series

Name	Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023

Conference

Conference	2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023
Country/Territory	China
City	Qingdao
Period	14/07/23 → 16/07/23

Keywords

High-order fully actuated system approach
Spacecraft attitude tracking
modified Rodrigues parameters

Access to Document

10.1109/CFASTA57821.2023.10243176

Cite this

Jin, D., Jia, S., Wang, T., & Qiu, J. (2023). Spacecraft Attitude Tracking Control Based on High-Order Fully Actuated System Approach. In Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023 (pp. 1040-1044). (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CFASTA57821.2023.10243176

Jin, Dongyan ; Jia, Shixiang ; Wang, Tong et al. / Spacecraft Attitude Tracking Control Based on High-Order Fully Actuated System Approach. Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc., 2023. pp. 1040-1044 (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023).

@inproceedings{bdbbce8ec6e84382acbaa05eb3ef1f15,

title = "Spacecraft Attitude Tracking Control Based on High-Order Fully Actuated System Approach",

abstract = "This paper focuses on the attitude tracking control of spacecraft. Firstly, the modified Rodrigues parameters are selected to characterize the spacecraft's attitude, whose mathematical model is then established by considering the uncertainties of the spacecraft parameters and the bounded disturbances. The mathematical model of the spacecraft is transformed into a type of high-order fully actuated (HOFA) system with uncertainties. Then, based on the HOFA system approach, a robust controller for a type of HOFA system with uncertainties is designed, which can ensure that the system states converge to an arbitrary ellipsoidal region. Finally, the validness of the designed controller is verified by simulation.",

keywords = "High-order fully actuated system approach, Spacecraft attitude tracking, modified Rodrigues parameters",

author = "Dongyan Jin and Shixiang Jia and Tong Wang and Jianbin Qiu",

note = "Publisher Copyright: {\textcopyright} 2023 IEEE.; 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023 ; Conference date: 14-07-2023 Through 16-07-2023",

year = "2023",

doi = "10.1109/CFASTA57821.2023.10243176",

language = "英语",

series = "Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023",

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

pages = "1040--1044",

booktitle = "Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023",

address = "美国",

}

Jin, D, Jia, S, Wang, T & Qiu, J 2023, Spacecraft Attitude Tracking Control Based on High-Order Fully Actuated System Approach. in Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023, Institute of Electrical and Electronics Engineers Inc., pp. 1040-1044, 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023, Qingdao, China, 14/07/23. https://doi.org/10.1109/CFASTA57821.2023.10243176

Spacecraft Attitude Tracking Control Based on High-Order Fully Actuated System Approach. / Jin, Dongyan; Jia, Shixiang; Wang, Tong et al.
Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc., 2023. p. 1040-1044 (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023).

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

TY - GEN

T1 - Spacecraft Attitude Tracking Control Based on High-Order Fully Actuated System Approach

AU - Jin, Dongyan

AU - Jia, Shixiang

AU - Wang, Tong

AU - Qiu, Jianbin

PY - 2023

Y1 - 2023

N2 - This paper focuses on the attitude tracking control of spacecraft. Firstly, the modified Rodrigues parameters are selected to characterize the spacecraft's attitude, whose mathematical model is then established by considering the uncertainties of the spacecraft parameters and the bounded disturbances. The mathematical model of the spacecraft is transformed into a type of high-order fully actuated (HOFA) system with uncertainties. Then, based on the HOFA system approach, a robust controller for a type of HOFA system with uncertainties is designed, which can ensure that the system states converge to an arbitrary ellipsoidal region. Finally, the validness of the designed controller is verified by simulation.

AB - This paper focuses on the attitude tracking control of spacecraft. Firstly, the modified Rodrigues parameters are selected to characterize the spacecraft's attitude, whose mathematical model is then established by considering the uncertainties of the spacecraft parameters and the bounded disturbances. The mathematical model of the spacecraft is transformed into a type of high-order fully actuated (HOFA) system with uncertainties. Then, based on the HOFA system approach, a robust controller for a type of HOFA system with uncertainties is designed, which can ensure that the system states converge to an arbitrary ellipsoidal region. Finally, the validness of the designed controller is verified by simulation.

KW - High-order fully actuated system approach

KW - Spacecraft attitude tracking

KW - modified Rodrigues parameters

UR - https://www.scopus.com/pages/publications/85173622340

U2 - 10.1109/CFASTA57821.2023.10243176

DO - 10.1109/CFASTA57821.2023.10243176

M3 - 会议稿件

AN - SCOPUS:85173622340

T3 - Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023

SP - 1040

EP - 1044

BT - Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023

Y2 - 14 July 2023 through 16 July 2023

ER -

Jin D, Jia S, Wang T , Qiu J. Spacecraft Attitude Tracking Control Based on High-Order Fully Actuated System Approach. In Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc. 2023. p. 1040-1044. (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023). doi: 10.1109/CFASTA57821.2023.10243176

Spacecraft Attitude Tracking Control Based on High-Order Fully Actuated System Approach

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