Predefined time sliding mode attitude tracking control for rigid spacecraft based on fully actuated system method

Yin Zheng; He Zhang; Yan Wang

doi:10.1109/FASTA61401.2024.10595263

Predefined time sliding mode attitude tracking control for rigid spacecraft based on fully actuated system method

Yin Zheng^*
, He Zhang
, Yan Wang

^*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

Based on the control theory of the fully actuated system method, this paper proposes a method of attitude-tracking control for rigid spacecraft by using a predefined time terminal sliding mode scheme. First, we establish the fully-actuated system model for the spacecraft by using the attitude dynamics and kinematics equation, then in order to improve the control efficiency, a new predefined time controller is designed by combining the fully actuated system method and the nonsingular terminal sliding mode control method. Finally, the effectiveness of the designed controller is verified by numerical simulation.

Original language	English
Title of host publication	Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1579-1583
Number of pages	5
ISBN (Electronic)	9798350373691
DOIs	https://doi.org/10.1109/FASTA61401.2024.10595263
State	Published - 2024
Externally published	Yes
Event	3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024 - Shenzhen, China Duration: 10 May 2024 → 12 May 2024

Publication series

Name	Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024

Conference

Conference	3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024
Country/Territory	China
City	Shenzhen
Period	10/05/24 → 12/05/24

Keywords

Attitude tracking
Fully actuated system method
Predefined time stability
Terminal sliding mode

Access to Document

10.1109/FASTA61401.2024.10595263

Cite this

Zheng, Y., Zhang, H., & Wang, Y. (2024). Predefined time sliding mode attitude tracking control for rigid spacecraft based on fully actuated system method. In Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024 (pp. 1579-1583). (Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/FASTA61401.2024.10595263

Zheng, Yin ; Zhang, He ; Wang, Yan. / Predefined time sliding mode attitude tracking control for rigid spacecraft based on fully actuated system method. Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024. Institute of Electrical and Electronics Engineers Inc., 2024. pp. 1579-1583 (Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024).

@inproceedings{ca1940c1b8224ec88fe751baf1419780,

title = "Predefined time sliding mode attitude tracking control for rigid spacecraft based on fully actuated system method",

abstract = "Based on the control theory of the fully actuated system method, this paper proposes a method of attitude-tracking control for rigid spacecraft by using a predefined time terminal sliding mode scheme. First, we establish the fully-actuated system model for the spacecraft by using the attitude dynamics and kinematics equation, then in order to improve the control efficiency, a new predefined time controller is designed by combining the fully actuated system method and the nonsingular terminal sliding mode control method. Finally, the effectiveness of the designed controller is verified by numerical simulation.",

keywords = "Attitude tracking, Fully actuated system method, Predefined time stability, Terminal sliding mode",

author = "Yin Zheng and He Zhang and Yan Wang",

note = "Publisher Copyright: {\textcopyright} 2024 IEEE.; 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024 ; Conference date: 10-05-2024 Through 12-05-2024",

year = "2024",

doi = "10.1109/FASTA61401.2024.10595263",

language = "英语",

series = "Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024",

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

pages = "1579--1583",

booktitle = "Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024",

address = "美国",

}

Zheng, Y, Zhang, H & Wang, Y 2024, Predefined time sliding mode attitude tracking control for rigid spacecraft based on fully actuated system method. in Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024. Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024, Institute of Electrical and Electronics Engineers Inc., pp. 1579-1583, 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024, Shenzhen, China, 10/05/24. https://doi.org/10.1109/FASTA61401.2024.10595263

Predefined time sliding mode attitude tracking control for rigid spacecraft based on fully actuated system method. / Zheng, Yin; Zhang, He; Wang, Yan.
Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024. Institute of Electrical and Electronics Engineers Inc., 2024. p. 1579-1583 (Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024).

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

TY - GEN

T1 - Predefined time sliding mode attitude tracking control for rigid spacecraft based on fully actuated system method

AU - Zheng, Yin

AU - Zhang, He

AU - Wang, Yan

PY - 2024

Y1 - 2024

N2 - Based on the control theory of the fully actuated system method, this paper proposes a method of attitude-tracking control for rigid spacecraft by using a predefined time terminal sliding mode scheme. First, we establish the fully-actuated system model for the spacecraft by using the attitude dynamics and kinematics equation, then in order to improve the control efficiency, a new predefined time controller is designed by combining the fully actuated system method and the nonsingular terminal sliding mode control method. Finally, the effectiveness of the designed controller is verified by numerical simulation.

AB - Based on the control theory of the fully actuated system method, this paper proposes a method of attitude-tracking control for rigid spacecraft by using a predefined time terminal sliding mode scheme. First, we establish the fully-actuated system model for the spacecraft by using the attitude dynamics and kinematics equation, then in order to improve the control efficiency, a new predefined time controller is designed by combining the fully actuated system method and the nonsingular terminal sliding mode control method. Finally, the effectiveness of the designed controller is verified by numerical simulation.

KW - Attitude tracking

KW - Fully actuated system method

KW - Predefined time stability

KW - Terminal sliding mode

UR - https://www.scopus.com/pages/publications/85200555454

U2 - 10.1109/FASTA61401.2024.10595263

DO - 10.1109/FASTA61401.2024.10595263

M3 - 会议稿件

AN - SCOPUS:85200555454

T3 - Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024

SP - 1579

EP - 1583

BT - Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024

Y2 - 10 May 2024 through 12 May 2024

ER -

Zheng Y, Zhang H, Wang Y. Predefined time sliding mode attitude tracking control for rigid spacecraft based on fully actuated system method. In Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024. Institute of Electrical and Electronics Engineers Inc. 2024. p. 1579-1583. (Proceedings of the 3rd Conference on Fully Actuated System Theory and Applications, FASTA 2024). doi: 10.1109/FASTA61401.2024.10595263

Predefined time sliding mode attitude tracking control for rigid spacecraft based on fully actuated system method

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this