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

Dongyan Jin; Mingyu Hou; Tong Wang; Jianbin Qiu

doi:10.1109/FASTA61401.2024.10595265

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

Dongyan Jin^*
, Mingyu Hou
, 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

2 Scopus citations

Abstract

In this paper, the adaptive attitude tracking control of spacecraft with unknown time-varying disturbances is studied. Firstly, the attitude model is established using modified Rodriguez parameters, which is transformed into a high-order fully actuated (HOFA) system model with unknown time-varying parameters. Then, a novel adaptive attitude tracking control strategy based on the HOFA system approach is proposed. With the proposed control strategy, the unknown time-varying disturbances are estimated and compensated. The system stability of spacecraft attitude is guaranteed via Lyapunov theory. Finally, the effectiveness of the proposed control strategy is verified through numerical simulations.

Original language	English
Title of host publication	Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1532-1537
Number of pages	6
ISBN (Electronic)	9798350373691
DOIs	https://doi.org/10.1109/FASTA61401.2024.10595265
State	Published - 2024
Event	3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024 - Shenzhen, China Duration: 10 May 2024 → 12 May 2024

Publication series

Name	Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024

Conference

Conference	3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024
Country/Territory	China
City	Shenzhen
Period	10/05/24 → 12/05/24

Keywords

Adaptive control
high-order fully actuated system approach
modified Rodrigues parameters
spacecraft attitude control

Access to Document

10.1109/FASTA61401.2024.10595265

Cite this

Jin, D., Hou, M., Wang, T., & Qiu, J. (2024). Adaptive Attitude Tracking Control of Spacecraft Based on High-Order Fully Actuated System Approach. In Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024 (pp. 1532-1537). (Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/FASTA61401.2024.10595265

Jin, Dongyan ; Hou, Mingyu ; Wang, Tong et al. / Adaptive Attitude Tracking Control of Spacecraft Based on High-Order Fully Actuated System Approach. Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024. Institute of Electrical and Electronics Engineers Inc., 2024. pp. 1532-1537 (Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024).

@inproceedings{37c84f30c6704a209a89967d819ebd3d,

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

abstract = "In this paper, the adaptive attitude tracking control of spacecraft with unknown time-varying disturbances is studied. Firstly, the attitude model is established using modified Rodriguez parameters, which is transformed into a high-order fully actuated (HOFA) system model with unknown time-varying parameters. Then, a novel adaptive attitude tracking control strategy based on the HOFA system approach is proposed. With the proposed control strategy, the unknown time-varying disturbances are estimated and compensated. The system stability of spacecraft attitude is guaranteed via Lyapunov theory. Finally, the effectiveness of the proposed control strategy is verified through numerical simulations.",

keywords = "Adaptive control, high-order fully actuated system approach, modified Rodrigues parameters, spacecraft attitude control",

author = "Dongyan Jin and Mingyu Hou and Tong Wang and Jianbin Qiu",

note = "Publisher Copyright: {\textcopyright} 2024 IEEE.; 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024 ; Conference date: 10-05-2024 Through 12-05-2024",

year = "2024",

doi = "10.1109/FASTA61401.2024.10595265",

language = "英语",

series = "Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024",

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

pages = "1532--1537",

booktitle = "Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024",

address = "美国",

}

Jin, D, Hou, M, Wang, T & Qiu, J 2024, Adaptive Attitude Tracking Control of Spacecraft Based on High-Order Fully Actuated System Approach. in Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024. Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024, Institute of Electrical and Electronics Engineers Inc., pp. 1532-1537, 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024, Shenzhen, China, 10/05/24. https://doi.org/10.1109/FASTA61401.2024.10595265

Adaptive Attitude Tracking Control of Spacecraft Based on High-Order Fully Actuated System Approach. / Jin, Dongyan; Hou, Mingyu; Wang, Tong et al.
Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024. Institute of Electrical and Electronics Engineers Inc., 2024. p. 1532-1537 (Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024).

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

TY - GEN

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

AU - Jin, Dongyan

AU - Hou, Mingyu

AU - Wang, Tong

AU - Qiu, Jianbin

PY - 2024

Y1 - 2024

N2 - In this paper, the adaptive attitude tracking control of spacecraft with unknown time-varying disturbances is studied. Firstly, the attitude model is established using modified Rodriguez parameters, which is transformed into a high-order fully actuated (HOFA) system model with unknown time-varying parameters. Then, a novel adaptive attitude tracking control strategy based on the HOFA system approach is proposed. With the proposed control strategy, the unknown time-varying disturbances are estimated and compensated. The system stability of spacecraft attitude is guaranteed via Lyapunov theory. Finally, the effectiveness of the proposed control strategy is verified through numerical simulations.

AB - In this paper, the adaptive attitude tracking control of spacecraft with unknown time-varying disturbances is studied. Firstly, the attitude model is established using modified Rodriguez parameters, which is transformed into a high-order fully actuated (HOFA) system model with unknown time-varying parameters. Then, a novel adaptive attitude tracking control strategy based on the HOFA system approach is proposed. With the proposed control strategy, the unknown time-varying disturbances are estimated and compensated. The system stability of spacecraft attitude is guaranteed via Lyapunov theory. Finally, the effectiveness of the proposed control strategy is verified through numerical simulations.

KW - Adaptive control

KW - high-order fully actuated system approach

KW - modified Rodrigues parameters

KW - spacecraft attitude control

UR - https://www.scopus.com/pages/publications/85200544399

U2 - 10.1109/FASTA61401.2024.10595265

DO - 10.1109/FASTA61401.2024.10595265

M3 - 会议稿件

AN - SCOPUS:85200544399

T3 - Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024

SP - 1532

EP - 1537

BT - Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024

Y2 - 10 May 2024 through 12 May 2024

ER -

Jin D, Hou M, Wang T , Qiu J. Adaptive Attitude Tracking Control of Spacecraft Based on High-Order Fully Actuated System Approach. In Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024. Institute of Electrical and Electronics Engineers Inc. 2024. p. 1532-1537. (Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024). doi: 10.1109/FASTA61401.2024.10595265

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

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