Underactuated Attitude Control of Three-Body Tethered Spacecraft During Spinning for Artificial Gravity

Tian Haochang; Li Linxiao; Li Aijun; Wang Changqing

doi:10.1007/978-981-19-6613-2_199

Underactuated Attitude Control of Three-Body Tethered Spacecraft During Spinning for Artificial Gravity

Tian Haochang, Li Linxiao, Li Aijun, Wang Changqing

School of Automation

Northwestern Polytechnical University Xian

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

Abstract

This work studies the spinning three-body tethered spacecraft to achieve the desired artificial gravity overload. To explain the rigid-flexible coupling characteristics of the tethered system, tethers are regarded as discrete mass points to build the mathematical model. The quaternion theory is used to describe coordinate system rotation to avoid the singularity problems of tethers and tethered spacecraft. An underactuated controller is proposed to control the attitudes of sub-spacecraft during spin-up. Then, the asymptotic stability of the tethered system with attitude error is proven. To deal with the influence of unknown bounded external disturbance on sub-spacecraft attitude, a disturbance estimation function with hyperbolic cosine type is designed to suppress system chattering. In the numerical simulation, the spin-up dynamic behavior of three-body tethered spacecraft without attitude control is studied. Finally, the effectiveness and robustness of the underactuated controller are demonstrated in the simulation.

Original language	English
Title of host publication	Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
Editors	Liang Yan, Haibin Duan, Yimin Deng, Liang Yan
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	2033-2042
Number of pages	10
ISBN (Print)	9789811966125
DOIs	https://doi.org/10.1007/978-981-19-6613-2_199
State	Published - 2023
Event	International Conference on Guidance, Navigation and Control, ICGNC 2022 - Harbin, China Duration: 5 Aug 2022 → 7 Aug 2022

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	845 LNEE
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	International Conference on Guidance, Navigation and Control, ICGNC 2022
Country/Territory	China
City	Harbin
Period	5/08/22 → 7/08/22

Keywords

Artificial gravity
Backstepping control
Spin-up
Three-body tethered spacecraft
Underactuated attitude system

Access to Document

10.1007/978-981-19-6613-2_199

Cite this

Haochang, T., Linxiao, L., Aijun, L., & Changqing, W. (2023). Underactuated Attitude Control of Three-Body Tethered Spacecraft During Spinning for Artificial Gravity. In L. Yan, H. Duan, Y. Deng, & L. Yan (Eds.), Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control (pp. 2033-2042). (Lecture Notes in Electrical Engineering; Vol. 845 LNEE). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-19-6613-2_199

Haochang, Tian ; Linxiao, Li ; Aijun, Li et al. / Underactuated Attitude Control of Three-Body Tethered Spacecraft During Spinning for Artificial Gravity. Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. editor / Liang Yan ; Haibin Duan ; Yimin Deng ; Liang Yan. Springer Science and Business Media Deutschland GmbH, 2023. pp. 2033-2042 (Lecture Notes in Electrical Engineering).

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title = "Underactuated Attitude Control of Three-Body Tethered Spacecraft During Spinning for Artificial Gravity",

abstract = "This work studies the spinning three-body tethered spacecraft to achieve the desired artificial gravity overload. To explain the rigid-flexible coupling characteristics of the tethered system, tethers are regarded as discrete mass points to build the mathematical model. The quaternion theory is used to describe coordinate system rotation to avoid the singularity problems of tethers and tethered spacecraft. An underactuated controller is proposed to control the attitudes of sub-spacecraft during spin-up. Then, the asymptotic stability of the tethered system with attitude error is proven. To deal with the influence of unknown bounded external disturbance on sub-spacecraft attitude, a disturbance estimation function with hyperbolic cosine type is designed to suppress system chattering. In the numerical simulation, the spin-up dynamic behavior of three-body tethered spacecraft without attitude control is studied. Finally, the effectiveness and robustness of the underactuated controller are demonstrated in the simulation.",

keywords = "Artificial gravity, Backstepping control, Spin-up, Three-body tethered spacecraft, Underactuated attitude system",

author = "Tian Haochang and Li Linxiao and Li Aijun and Wang Changqing",

note = "Publisher Copyright: {\textcopyright} 2023, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.; International Conference on Guidance, Navigation and Control, ICGNC 2022 ; Conference date: 05-08-2022 Through 07-08-2022",

year = "2023",

doi = "10.1007/978-981-19-6613-2_199",

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Haochang, T, Linxiao, L, Aijun, L & Changqing, W 2023, Underactuated Attitude Control of Three-Body Tethered Spacecraft During Spinning for Artificial Gravity. in L Yan, H Duan, Y Deng & L Yan (eds), Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. Lecture Notes in Electrical Engineering, vol. 845 LNEE, Springer Science and Business Media Deutschland GmbH, pp. 2033-2042, International Conference on Guidance, Navigation and Control, ICGNC 2022, Harbin, China, 5/08/22. https://doi.org/10.1007/978-981-19-6613-2_199

Underactuated Attitude Control of Three-Body Tethered Spacecraft During Spinning for Artificial Gravity. / Haochang, Tian; Linxiao, Li; Aijun, Li et al.
Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. ed. / Liang Yan; Haibin Duan; Yimin Deng; Liang Yan. Springer Science and Business Media Deutschland GmbH, 2023. p. 2033-2042 (Lecture Notes in Electrical Engineering; Vol. 845 LNEE).

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

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PY - 2023

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N2 - This work studies the spinning three-body tethered spacecraft to achieve the desired artificial gravity overload. To explain the rigid-flexible coupling characteristics of the tethered system, tethers are regarded as discrete mass points to build the mathematical model. The quaternion theory is used to describe coordinate system rotation to avoid the singularity problems of tethers and tethered spacecraft. An underactuated controller is proposed to control the attitudes of sub-spacecraft during spin-up. Then, the asymptotic stability of the tethered system with attitude error is proven. To deal with the influence of unknown bounded external disturbance on sub-spacecraft attitude, a disturbance estimation function with hyperbolic cosine type is designed to suppress system chattering. In the numerical simulation, the spin-up dynamic behavior of three-body tethered spacecraft without attitude control is studied. Finally, the effectiveness and robustness of the underactuated controller are demonstrated in the simulation.

AB - This work studies the spinning three-body tethered spacecraft to achieve the desired artificial gravity overload. To explain the rigid-flexible coupling characteristics of the tethered system, tethers are regarded as discrete mass points to build the mathematical model. The quaternion theory is used to describe coordinate system rotation to avoid the singularity problems of tethers and tethered spacecraft. An underactuated controller is proposed to control the attitudes of sub-spacecraft during spin-up. Then, the asymptotic stability of the tethered system with attitude error is proven. To deal with the influence of unknown bounded external disturbance on sub-spacecraft attitude, a disturbance estimation function with hyperbolic cosine type is designed to suppress system chattering. In the numerical simulation, the spin-up dynamic behavior of three-body tethered spacecraft without attitude control is studied. Finally, the effectiveness and robustness of the underactuated controller are demonstrated in the simulation.

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PB - Springer Science and Business Media Deutschland GmbH

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Y2 - 5 August 2022 through 7 August 2022

ER -

Haochang T, Linxiao L, Aijun L, Changqing W. Underactuated Attitude Control of Three-Body Tethered Spacecraft During Spinning for Artificial Gravity. In Yan L, Duan H, Deng Y, Yan L, editors, Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control. Springer Science and Business Media Deutschland GmbH. 2023. p. 2033-2042. (Lecture Notes in Electrical Engineering). doi: 10.1007/978-981-19-6613-2_199

Underactuated Attitude Control of Three-Body Tethered Spacecraft During Spinning for Artificial Gravity

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