Prescribed Performance Control for Attitude Tracking of Spacecraft via High-Order Fully Actuated System Approach and Extended State Observer

Dongyan Jin; Tianhao Zhang; Yichuan Fu; Jianbin Qiu

doi:10.1109/FASTA65681.2025.11138573

Prescribed Performance Control for Attitude Tracking of Spacecraft via High-Order Fully Actuated System Approach and Extended State Observer

Dongyan Jin
, Tianhao Zhang
, Yichuan Fu
, Jianbin Qiu

School of Astronautics

Harbin Institute of Technology

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

Abstract

This paper addresses the problem of prescribed performance control for attitude tracking of spacecraft under external disturbances. First, a high-order fully actuated system model is established through state transformation based on the prescribed performance function. An extended state observer is designed to estimate and compensate for unknown disturbance terms. Then, a novel controller based on the high-order fully actuated system approach is proposed to ensure stability of system. Finally, simulation results validate the effectiveness of the proposed controller.

Original language	English
Title of host publication	Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	343-347
Number of pages	5
ISBN (Electronic)	9798331526924
DOIs	https://doi.org/10.1109/FASTA65681.2025.11138573
State	Published - 2025
Event	4th Conference on Fully Actuated System Theory and Applications, FASTA 2025 - Nanjing, China Duration: 4 Jul 2025 → 6 Jul 2025

Publication series

Name	Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025

Conference

Conference	4th Conference on Fully Actuated System Theory and Applications, FASTA 2025
Country/Territory	China
City	Nanjing
Period	4/07/25 → 6/07/25

Keywords

Prescribed performance control
extended state observer
high-order fully actuated system approach
spacecraft attitude control

Access to Document

10.1109/FASTA65681.2025.11138573

Cite this

Jin, D., Zhang, T., Fu, Y., & Qiu, J. (2025). Prescribed Performance Control for Attitude Tracking of Spacecraft via High-Order Fully Actuated System Approach and Extended State Observer. In Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025 (pp. 343-347). (Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/FASTA65681.2025.11138573

Jin, Dongyan ; Zhang, Tianhao ; Fu, Yichuan et al. / Prescribed Performance Control for Attitude Tracking of Spacecraft via High-Order Fully Actuated System Approach and Extended State Observer. Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025. Institute of Electrical and Electronics Engineers Inc., 2025. pp. 343-347 (Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025).

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title = "Prescribed Performance Control for Attitude Tracking of Spacecraft via High-Order Fully Actuated System Approach and Extended State Observer",

abstract = "This paper addresses the problem of prescribed performance control for attitude tracking of spacecraft under external disturbances. First, a high-order fully actuated system model is established through state transformation based on the prescribed performance function. An extended state observer is designed to estimate and compensate for unknown disturbance terms. Then, a novel controller based on the high-order fully actuated system approach is proposed to ensure stability of system. Finally, simulation results validate the effectiveness of the proposed controller.",

keywords = "Prescribed performance control, extended state observer, high-order fully actuated system approach, spacecraft attitude control",

author = "Dongyan Jin and Tianhao Zhang and Yichuan Fu and Jianbin Qiu",

note = "Publisher Copyright: {\textcopyright} 2025 IEEE.; 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025 ; Conference date: 04-07-2025 Through 06-07-2025",

year = "2025",

doi = "10.1109/FASTA65681.2025.11138573",

language = "英语",

series = "Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025",

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

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Jin, D, Zhang, T, Fu, Y & Qiu, J 2025, Prescribed Performance Control for Attitude Tracking of Spacecraft via High-Order Fully Actuated System Approach and Extended State Observer. in Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025. Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025, Institute of Electrical and Electronics Engineers Inc., pp. 343-347, 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025, Nanjing, China, 4/07/25. https://doi.org/10.1109/FASTA65681.2025.11138573

Prescribed Performance Control for Attitude Tracking of Spacecraft via High-Order Fully Actuated System Approach and Extended State Observer. / Jin, Dongyan; Zhang, Tianhao; Fu, Yichuan et al.
Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025. Institute of Electrical and Electronics Engineers Inc., 2025. p. 343-347 (Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025).

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

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PY - 2025

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N2 - This paper addresses the problem of prescribed performance control for attitude tracking of spacecraft under external disturbances. First, a high-order fully actuated system model is established through state transformation based on the prescribed performance function. An extended state observer is designed to estimate and compensate for unknown disturbance terms. Then, a novel controller based on the high-order fully actuated system approach is proposed to ensure stability of system. Finally, simulation results validate the effectiveness of the proposed controller.

AB - This paper addresses the problem of prescribed performance control for attitude tracking of spacecraft under external disturbances. First, a high-order fully actuated system model is established through state transformation based on the prescribed performance function. An extended state observer is designed to estimate and compensate for unknown disturbance terms. Then, a novel controller based on the high-order fully actuated system approach is proposed to ensure stability of system. Finally, simulation results validate the effectiveness of the proposed controller.

KW - Prescribed performance control

KW - extended state observer

KW - high-order fully actuated system approach

KW - spacecraft attitude control

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PB - Institute of Electrical and Electronics Engineers Inc.

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Jin D, Zhang T, Fu Y, Qiu J. Prescribed Performance Control for Attitude Tracking of Spacecraft via High-Order Fully Actuated System Approach and Extended State Observer. In Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025. Institute of Electrical and Electronics Engineers Inc. 2025. p. 343-347. (Proceedings of the 4th Conference on Fully Actuated System Theory and Applications, FASTA 2025). doi: 10.1109/FASTA65681.2025.11138573

Prescribed Performance Control for Attitude Tracking of Spacecraft via High-Order Fully Actuated System Approach and Extended State Observer

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