Fully-Actuated-system-Approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying

Jiao Wu; Yuehua Liu; Ming Liu; Xibin Cao

doi:10.1109/CFASTA57821.2023.10243360

Fully-Actuated-system-Approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying

Jiao Wu^*
, Yuehua Liu
, Ming Liu
, Xibin Cao

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

3 Scopus citations

Abstract

In this paper, an attitude-orbit integrated control law based on the fully-Actuated system approach is proposed for spacecraft formation flying system. A 6DOF attitude-orbit integrated kinematic and dynamic model based on SE(3) description is established, and the fully-Actuated system model is derived. Considering the effects of disturbances and unknown items of model, an adaptive neural network is designed to compensate the effects. Further, a fully-Actuated-system-Approach-based controller is developed for spacecraft formation flying tasks. The convergency of formation tracking error is proved via the Lyapunov stability theory. Finally, numerical results indicate the effectiveness of the control law proposed in this paper.

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	717-722
Number of pages	6
ISBN (Electronic)	9798350332162
DOIs	https://doi.org/10.1109/CFASTA57821.2023.10243360
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

Fully-Actuated system approach
SE(3)
adaptive neural network
attitude-orbit integrated control
spacecraft formation flying

Access to Document

10.1109/CFASTA57821.2023.10243360

Cite this

Wu, J., Liu, Y., Liu, M., & Cao, X. (2023). Fully-Actuated-system-Approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying. In Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023 (pp. 717-722). (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/CFASTA57821.2023.10243360

Wu, Jiao ; Liu, Yuehua ; Liu, Ming et al. / Fully-Actuated-system-Approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying. Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc., 2023. pp. 717-722 (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023).

@inproceedings{e41757bd8f964ff6bd6f83e78695eeff,

title = "Fully-Actuated-system-Approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying",

abstract = "In this paper, an attitude-orbit integrated control law based on the fully-Actuated system approach is proposed for spacecraft formation flying system. A 6DOF attitude-orbit integrated kinematic and dynamic model based on SE(3) description is established, and the fully-Actuated system model is derived. Considering the effects of disturbances and unknown items of model, an adaptive neural network is designed to compensate the effects. Further, a fully-Actuated-system-Approach-based controller is developed for spacecraft formation flying tasks. The convergency of formation tracking error is proved via the Lyapunov stability theory. Finally, numerical results indicate the effectiveness of the control law proposed in this paper.",

keywords = "Fully-Actuated system approach, SE(3), adaptive neural network, attitude-orbit integrated control, spacecraft formation flying",

author = "Jiao Wu and Yuehua Liu and Ming Liu and Xibin Cao",

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/CFASTA57821.2023.10243360",

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 = "717--722",

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

address = "美国",

}

Wu, J, Liu, Y, Liu, M & Cao, X 2023, Fully-Actuated-system-Approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying. 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. 717-722, 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023, Qingdao, China, 14/07/23. https://doi.org/10.1109/CFASTA57821.2023.10243360

Fully-Actuated-system-Approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying. / Wu, Jiao; Liu, Yuehua; Liu, Ming 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. 717-722 (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 - Fully-Actuated-system-Approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying

AU - Wu, Jiao

AU - Liu, Yuehua

AU - Liu, Ming

AU - Cao, Xibin

PY - 2023

Y1 - 2023

N2 - In this paper, an attitude-orbit integrated control law based on the fully-Actuated system approach is proposed for spacecraft formation flying system. A 6DOF attitude-orbit integrated kinematic and dynamic model based on SE(3) description is established, and the fully-Actuated system model is derived. Considering the effects of disturbances and unknown items of model, an adaptive neural network is designed to compensate the effects. Further, a fully-Actuated-system-Approach-based controller is developed for spacecraft formation flying tasks. The convergency of formation tracking error is proved via the Lyapunov stability theory. Finally, numerical results indicate the effectiveness of the control law proposed in this paper.

AB - In this paper, an attitude-orbit integrated control law based on the fully-Actuated system approach is proposed for spacecraft formation flying system. A 6DOF attitude-orbit integrated kinematic and dynamic model based on SE(3) description is established, and the fully-Actuated system model is derived. Considering the effects of disturbances and unknown items of model, an adaptive neural network is designed to compensate the effects. Further, a fully-Actuated-system-Approach-based controller is developed for spacecraft formation flying tasks. The convergency of formation tracking error is proved via the Lyapunov stability theory. Finally, numerical results indicate the effectiveness of the control law proposed in this paper.

KW - Fully-Actuated system approach

KW - SE(3)

KW - adaptive neural network

KW - attitude-orbit integrated control

KW - spacecraft formation flying

UR - https://www.scopus.com/pages/publications/85173602952

U2 - 10.1109/CFASTA57821.2023.10243360

DO - 10.1109/CFASTA57821.2023.10243360

M3 - 会议稿件

AN - SCOPUS:85173602952

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

SP - 717

EP - 722

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 -

Wu J, Liu Y, Liu M , Cao X. Fully-Actuated-system-Approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying. In Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023. Institute of Electrical and Electronics Engineers Inc. 2023. p. 717-722. (Proceedings of the 2nd Conference on Fully Actuated System Theory and Applications, CFASTA 2023). doi: 10.1109/CFASTA57821.2023.10243360

Fully-Actuated-system-Approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying

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