Fully-Actuated-System-Based Fault-Tolerant Spacecraft Attitude Control with ESO

Tao Huo; Yang Yu; Chengfei Yue; Xueqin Chen

doi:10.1109/FASTA70174.2026.11548803

Fully-Actuated-System-Based Fault-Tolerant Spacecraft Attitude Control with ESO

Tao Huo
, Yang Yu
, Chengfei Yue
, Xueqin Chen

State Key Laboratory of Micro-Spacecraft Rapid Design and Intelligent Cluster
Shanghai Electro-Mechanical Engineering Institute
National Key Laboratory of Automatic Target Recognition
Harbin Institute of Technology Shenzhen

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

Abstract

This paper investigates fault-tolerant attitude control for rigid spacecraft subject to actuator faults and external disturbances. A novel control scheme combining the fully actuated system (FAS) approach and a linear extended state observer (ESO) is proposed. Actuator faults and disturbances are treated as a lumped term, which is accurately estimated by the ESO and compensated in the FAS-based control law. The input-to-state stability (ISS) of the closed-loop system is rigorously established. Simulation results demonstrate that the proposed scheme provides robustness and high-precision attitude control performance under multiple uncertainties.

Original language	English
Title of host publication	Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	201-205
Number of pages	5
ISBN (Electronic)	9798319547323
DOIs	https://doi.org/10.1109/FASTA70174.2026.11548803
State	Published - 2026
Externally published	Yes
Event	5th Conference on Fully Actuated System Theory and Applications, FASTA 2026 - Qinhuangdao, China Duration: 22 May 2026 → 24 May 2026

Publication series

Name	Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026

Conference

Conference	5th Conference on Fully Actuated System Theory and Applications, FASTA 2026
Country/Territory	China
City	Qinhuangdao
Period	22/05/26 → 24/05/26

Keywords

Extended State Observer
Fault Tolerant Control
Fully Actuated System
Spacecraft Attitude Control

Access to Document

10.1109/FASTA70174.2026.11548803

Cite this

Huo, T., Yu, Y., Yue, C., & Chen, X. (2026). Fully-Actuated-System-Based Fault-Tolerant Spacecraft Attitude Control with ESO. In Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026 (pp. 201-205). (Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/FASTA70174.2026.11548803

Huo, Tao ; Yu, Yang ; Yue, Chengfei et al. / Fully-Actuated-System-Based Fault-Tolerant Spacecraft Attitude Control with ESO. Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026. Institute of Electrical and Electronics Engineers Inc., 2026. pp. 201-205 (Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026).

@inproceedings{bcaf8567853a42ab8461860eba9e2190,

title = "Fully-Actuated-System-Based Fault-Tolerant Spacecraft Attitude Control with ESO",

abstract = "This paper investigates fault-tolerant attitude control for rigid spacecraft subject to actuator faults and external disturbances. A novel control scheme combining the fully actuated system (FAS) approach and a linear extended state observer (ESO) is proposed. Actuator faults and disturbances are treated as a lumped term, which is accurately estimated by the ESO and compensated in the FAS-based control law. The input-to-state stability (ISS) of the closed-loop system is rigorously established. Simulation results demonstrate that the proposed scheme provides robustness and high-precision attitude control performance under multiple uncertainties.",

keywords = "Extended State Observer, Fault Tolerant Control, Fully Actuated System, Spacecraft Attitude Control",

author = "Tao Huo and Yang Yu and Chengfei Yue and Xueqin Chen",

note = "Publisher Copyright: {\textcopyright} 2026 IEEE.; 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026 ; Conference date: 22-05-2026 Through 24-05-2026",

year = "2026",

doi = "10.1109/FASTA70174.2026.11548803",

language = "英语",

series = "Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026",

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

pages = "201--205",

booktitle = "Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026",

address = "美国",

}

Huo, T, Yu, Y, Yue, C & Chen, X 2026, Fully-Actuated-System-Based Fault-Tolerant Spacecraft Attitude Control with ESO. in Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026. Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026, Institute of Electrical and Electronics Engineers Inc., pp. 201-205, 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026, Qinhuangdao, China, 22/05/26. https://doi.org/10.1109/FASTA70174.2026.11548803

Fully-Actuated-System-Based Fault-Tolerant Spacecraft Attitude Control with ESO. / Huo, Tao; Yu, Yang; Yue, Chengfei et al.
Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026. Institute of Electrical and Electronics Engineers Inc., 2026. p. 201-205 (Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026).

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

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AU - Yue, Chengfei

AU - Chen, Xueqin

PY - 2026

Y1 - 2026

N2 - This paper investigates fault-tolerant attitude control for rigid spacecraft subject to actuator faults and external disturbances. A novel control scheme combining the fully actuated system (FAS) approach and a linear extended state observer (ESO) is proposed. Actuator faults and disturbances are treated as a lumped term, which is accurately estimated by the ESO and compensated in the FAS-based control law. The input-to-state stability (ISS) of the closed-loop system is rigorously established. Simulation results demonstrate that the proposed scheme provides robustness and high-precision attitude control performance under multiple uncertainties.

AB - This paper investigates fault-tolerant attitude control for rigid spacecraft subject to actuator faults and external disturbances. A novel control scheme combining the fully actuated system (FAS) approach and a linear extended state observer (ESO) is proposed. Actuator faults and disturbances are treated as a lumped term, which is accurately estimated by the ESO and compensated in the FAS-based control law. The input-to-state stability (ISS) of the closed-loop system is rigorously established. Simulation results demonstrate that the proposed scheme provides robustness and high-precision attitude control performance under multiple uncertainties.

KW - Extended State Observer

KW - Fault Tolerant Control

KW - Fully Actuated System

KW - Spacecraft Attitude Control

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BT - Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026

PB - Institute of Electrical and Electronics Engineers Inc.

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Huo T, Yu Y, Yue C, Chen X. Fully-Actuated-System-Based Fault-Tolerant Spacecraft Attitude Control with ESO. In Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026. Institute of Electrical and Electronics Engineers Inc. 2026. p. 201-205. (Proceedings of the 5th Conference on Fully Actuated System Theory and Applications, FASTA 2026). doi: 10.1109/FASTA70174.2026.11548803

Fully-Actuated-System-Based Fault-Tolerant Spacecraft Attitude Control with ESO

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