Optimal Attitude Takeover Control of Failed Spacecraft with Model Uncertainties

Qinwen Li; Zhongjie Meng

doi:10.1109/ICIEA54703.2022.10006034

Optimal Attitude Takeover Control of Failed Spacecraft with Model Uncertainties

Qinwen Li, Zhongjie Meng

School of Astronautics

Northwestern Polytechnical University Xian

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

2 Scopus citations

Abstract

In on-orbit service, attitude takeover control of failed spacecraft is a prerequisite of numerous tasks, such as on-orbit maintenance and on-orbit life extension. In takeover control missions, fuel consumption is a core key metric. Accordingly, attitude takeover control of spacecraft with model uncertainties with the minimum fuel consumption is studied in this paper. Concentrated on the optimal fuel consumption takeover control of failed spacecraft by nanosatellites, a control method based on fuzzy theory and inverse optimal control principle is proposed. Firstly, an auxiliary nonlinear system is constructed. Then on the basis of this auxiliary system, fuzzy logic systems (FLSs) are utilized to estimate the unknown nonlinear dynamics. Finally, combined with the inverse optimal principle and adaptive backstepping design theory, an optimal control law is designed. Numerical simulations are carried out to demonstrate the feasibility and effectiveness of the proposed control method.

Original language	English
Title of host publication	ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications
Editors	Wenxiang Xie, Shibin Gao, Xiaoqiong He, Xing Zhu, Jingjing Huang, Weirong Chen, Lei Ma, Haiyan Shu, Wenping Cao, Lijun Jiang, Zeliang Shu
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	213-218
Number of pages	6
ISBN (Electronic)	9781665409841
DOIs	https://doi.org/10.1109/ICIEA54703.2022.10006034
State	Published - 2022
Event	17th IEEE Conference on Industrial Electronics and Applications, ICIEA 2022 - Chengdu, China Duration: 16 Dec 2022 → 19 Dec 2022

Publication series

Name	ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications

Conference

Conference	17th IEEE Conference on Industrial Electronics and Applications, ICIEA 2022
Country/Territory	China
City	Chengdu
Period	16/12/22 → 19/12/22

Keywords

attitude takeover control
failed spacecraft
fuzzy adaptive control
inverse optimal control
model uncertainties

Access to Document

10.1109/ICIEA54703.2022.10006034

Cite this

Li, Q., & Meng, Z. (2022). Optimal Attitude Takeover Control of Failed Spacecraft with Model Uncertainties. In W. Xie, S. Gao, X. He, X. Zhu, J. Huang, W. Chen, L. Ma, H. Shu, W. Cao, L. Jiang, & Z. Shu (Eds.), ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications (pp. 213-218). (ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICIEA54703.2022.10006034

Li, Qinwen ; Meng, Zhongjie. / Optimal Attitude Takeover Control of Failed Spacecraft with Model Uncertainties. ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications. editor / Wenxiang Xie ; Shibin Gao ; Xiaoqiong He ; Xing Zhu ; Jingjing Huang ; Weirong Chen ; Lei Ma ; Haiyan Shu ; Wenping Cao ; Lijun Jiang ; Zeliang Shu. Institute of Electrical and Electronics Engineers Inc., 2022. pp. 213-218 (ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications).

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title = "Optimal Attitude Takeover Control of Failed Spacecraft with Model Uncertainties",

abstract = "In on-orbit service, attitude takeover control of failed spacecraft is a prerequisite of numerous tasks, such as on-orbit maintenance and on-orbit life extension. In takeover control missions, fuel consumption is a core key metric. Accordingly, attitude takeover control of spacecraft with model uncertainties with the minimum fuel consumption is studied in this paper. Concentrated on the optimal fuel consumption takeover control of failed spacecraft by nanosatellites, a control method based on fuzzy theory and inverse optimal control principle is proposed. Firstly, an auxiliary nonlinear system is constructed. Then on the basis of this auxiliary system, fuzzy logic systems (FLSs) are utilized to estimate the unknown nonlinear dynamics. Finally, combined with the inverse optimal principle and adaptive backstepping design theory, an optimal control law is designed. Numerical simulations are carried out to demonstrate the feasibility and effectiveness of the proposed control method.",

keywords = "attitude takeover control, failed spacecraft, fuzzy adaptive control, inverse optimal control, model uncertainties",

author = "Qinwen Li and Zhongjie Meng",

note = "Publisher Copyright: {\textcopyright} 2022 IEEE.; 17th IEEE Conference on Industrial Electronics and Applications, ICIEA 2022 ; Conference date: 16-12-2022 Through 19-12-2022",

year = "2022",

doi = "10.1109/ICIEA54703.2022.10006034",

language = "英语",

series = "ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications",

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

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editor = "Wenxiang Xie and Shibin Gao and Xiaoqiong He and Xing Zhu and Jingjing Huang and Weirong Chen and Lei Ma and Haiyan Shu and Wenping Cao and Lijun Jiang and Zeliang Shu",

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Li, Q & Meng, Z 2022, Optimal Attitude Takeover Control of Failed Spacecraft with Model Uncertainties. in W Xie, S Gao, X He, X Zhu, J Huang, W Chen, L Ma, H Shu, W Cao, L Jiang & Z Shu (eds), ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications. ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications, Institute of Electrical and Electronics Engineers Inc., pp. 213-218, 17th IEEE Conference on Industrial Electronics and Applications, ICIEA 2022, Chengdu, China, 16/12/22. https://doi.org/10.1109/ICIEA54703.2022.10006034

Optimal Attitude Takeover Control of Failed Spacecraft with Model Uncertainties. / Li, Qinwen; Meng, Zhongjie.
ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications. ed. / Wenxiang Xie; Shibin Gao; Xiaoqiong He; Xing Zhu; Jingjing Huang; Weirong Chen; Lei Ma; Haiyan Shu; Wenping Cao; Lijun Jiang; Zeliang Shu. Institute of Electrical and Electronics Engineers Inc., 2022. p. 213-218 (ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications).

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

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AU - Meng, Zhongjie

PY - 2022

Y1 - 2022

N2 - In on-orbit service, attitude takeover control of failed spacecraft is a prerequisite of numerous tasks, such as on-orbit maintenance and on-orbit life extension. In takeover control missions, fuel consumption is a core key metric. Accordingly, attitude takeover control of spacecraft with model uncertainties with the minimum fuel consumption is studied in this paper. Concentrated on the optimal fuel consumption takeover control of failed spacecraft by nanosatellites, a control method based on fuzzy theory and inverse optimal control principle is proposed. Firstly, an auxiliary nonlinear system is constructed. Then on the basis of this auxiliary system, fuzzy logic systems (FLSs) are utilized to estimate the unknown nonlinear dynamics. Finally, combined with the inverse optimal principle and adaptive backstepping design theory, an optimal control law is designed. Numerical simulations are carried out to demonstrate the feasibility and effectiveness of the proposed control method.

AB - In on-orbit service, attitude takeover control of failed spacecraft is a prerequisite of numerous tasks, such as on-orbit maintenance and on-orbit life extension. In takeover control missions, fuel consumption is a core key metric. Accordingly, attitude takeover control of spacecraft with model uncertainties with the minimum fuel consumption is studied in this paper. Concentrated on the optimal fuel consumption takeover control of failed spacecraft by nanosatellites, a control method based on fuzzy theory and inverse optimal control principle is proposed. Firstly, an auxiliary nonlinear system is constructed. Then on the basis of this auxiliary system, fuzzy logic systems (FLSs) are utilized to estimate the unknown nonlinear dynamics. Finally, combined with the inverse optimal principle and adaptive backstepping design theory, an optimal control law is designed. Numerical simulations are carried out to demonstrate the feasibility and effectiveness of the proposed control method.

KW - attitude takeover control

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KW - inverse optimal control

KW - model uncertainties

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BT - ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications

A2 - Xie, Wenxiang

A2 - Gao, Shibin

A2 - He, Xiaoqiong

A2 - Zhu, Xing

A2 - Huang, Jingjing

A2 - Chen, Weirong

A2 - Ma, Lei

A2 - Shu, Haiyan

A2 - Cao, Wenping

A2 - Jiang, Lijun

A2 - Shu, Zeliang

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 17th IEEE Conference on Industrial Electronics and Applications, ICIEA 2022

Y2 - 16 December 2022 through 19 December 2022

ER -

Li Q, Meng Z. Optimal Attitude Takeover Control of Failed Spacecraft with Model Uncertainties. In Xie W, Gao S, He X, Zhu X, Huang J, Chen W, Ma L, Shu H, Cao W, Jiang L, Shu Z, editors, ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications. Institute of Electrical and Electronics Engineers Inc. 2022. p. 213-218. (ICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications). doi: 10.1109/ICIEA54703.2022.10006034

Optimal Attitude Takeover Control of Failed Spacecraft with Model Uncertainties

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Keywords

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