ADP-Based Prescribed Performance Attitude Tracking Control for Rigid Spacecraft

Haoyang Yang; Yizhong Fang; Ming Guo; Bo Zhang; Yonghe Zhang; Qinglei Hu

doi:10.1109/CCDC52312.2021.9602522

ADP-Based Prescribed Performance Attitude Tracking Control for Rigid Spacecraft

Haoyang Yang
, Yizhong Fang
, Ming Guo
, Bo Zhang
, Yonghe Zhang
, Qinglei Hu^*

^*此作品的通讯作者

自动化科学与电气工程学院

Beihang University
The State Key Laboratory of Experiment Physics and Computational Mathematic
Beijing Institute of Space Long March Vehicle
Chinese Academy of Sciences
CAS - Innovation Academy for Microsatellites

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

6 引用（Scopus）

摘要

This paper proposes an adaptive dynamic programming (ADP)-based prescribed performance controller for rigid spacecraft attitude tracking control subject to cost optimizing. As a stepping stone, the modified Rodrigues Parameters (MRPs) are employed to characterize the relative attitude dynamics. A state transformation method is used to transform the constrained dynamics to an unconstrained dynamics by the log-type function. Then, an ADP algorithm is developed to deal with the Hamilton-Jacobi-Bellman equation of optimal control problem. The convergence and stability are analyzed by the Lyapunov-based method. Finally, the effectiveness of the proposed scheme is demonstrated by numerical simulation.

源语言	英语
主期刊名	Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021
出版商	Institute of Electrical and Electronics Engineers Inc.
页	6121-6126
页数	6
ISBN（电子版）	9781665440899
DOI	https://doi.org/10.1109/CCDC52312.2021.9602522
出版状态	已出版 - 2021
活动	33rd Chinese Control and Decision Conference, CCDC 2021 - Kunming, 中国期限: 22 5月 2021 → 24 5月 2021

出版系列

姓名	Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021

会议

会议	33rd Chinese Control and Decision Conference, CCDC 2021
国家/地区	中国
市	Kunming
时期	22/05/21 → 24/05/21

访问文件

10.1109/CCDC52312.2021.9602522

其它文件与链接

链接到 Scopus 的出版物

引用此

Yang, H., Fang, Y., Guo, M., Zhang, B., Zhang, Y., & Hu, Q. (2021). ADP-Based Prescribed Performance Attitude Tracking Control for Rigid Spacecraft. 在 Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021 (页码 6121-6126). (Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC52312.2021.9602522

@inproceedings{64e6a01e91104cc0a2d51b9d23aa99bc,

title = "ADP-Based Prescribed Performance Attitude Tracking Control for Rigid Spacecraft",

abstract = "This paper proposes an adaptive dynamic programming (ADP)-based prescribed performance controller for rigid spacecraft attitude tracking control subject to cost optimizing. As a stepping stone, the modified Rodrigues Parameters (MRPs) are employed to characterize the relative attitude dynamics. A state transformation method is used to transform the constrained dynamics to an unconstrained dynamics by the log-type function. Then, an ADP algorithm is developed to deal with the Hamilton-Jacobi-Bellman equation of optimal control problem. The convergence and stability are analyzed by the Lyapunov-based method. Finally, the effectiveness of the proposed scheme is demonstrated by numerical simulation.",

keywords = "Adaptive Dynamic Programming (ADP), Prescribed Performance Control, Reinforcement Learning, Spacecraft Attitude Control",

author = "Haoyang Yang and Yizhong Fang and Ming Guo and Bo Zhang and Yonghe Zhang and Qinglei Hu",

note = "Publisher Copyright: {\textcopyright} 2021 IEEE.; 33rd Chinese Control and Decision Conference, CCDC 2021 ; Conference date: 22-05-2021 Through 24-05-2021",

year = "2021",

doi = "10.1109/CCDC52312.2021.9602522",

language = "英语",

series = "Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021",

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

pages = "6121--6126",

booktitle = "Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021",

address = "美国",

}

Yang, H, Fang, Y, Guo, M, Zhang, B, Zhang, Y & Hu, Q 2021, ADP-Based Prescribed Performance Attitude Tracking Control for Rigid Spacecraft. 在 Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021. Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021, Institute of Electrical and Electronics Engineers Inc., 页码 6121-6126, 33rd Chinese Control and Decision Conference, CCDC 2021, Kunming, 中国, 22/05/21. https://doi.org/10.1109/CCDC52312.2021.9602522

ADP-Based Prescribed Performance Attitude Tracking Control for Rigid Spacecraft. / Yang, Haoyang; Fang, Yizhong; Guo, Ming 等.
Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021. Institute of Electrical and Electronics Engineers Inc., 2021. 页码 6121-6126 (Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

TY - GEN

T1 - ADP-Based Prescribed Performance Attitude Tracking Control for Rigid Spacecraft

AU - Yang, Haoyang

AU - Fang, Yizhong

AU - Guo, Ming

AU - Zhang, Bo

AU - Zhang, Yonghe

AU - Hu, Qinglei

PY - 2021

Y1 - 2021

N2 - This paper proposes an adaptive dynamic programming (ADP)-based prescribed performance controller for rigid spacecraft attitude tracking control subject to cost optimizing. As a stepping stone, the modified Rodrigues Parameters (MRPs) are employed to characterize the relative attitude dynamics. A state transformation method is used to transform the constrained dynamics to an unconstrained dynamics by the log-type function. Then, an ADP algorithm is developed to deal with the Hamilton-Jacobi-Bellman equation of optimal control problem. The convergence and stability are analyzed by the Lyapunov-based method. Finally, the effectiveness of the proposed scheme is demonstrated by numerical simulation.

AB - This paper proposes an adaptive dynamic programming (ADP)-based prescribed performance controller for rigid spacecraft attitude tracking control subject to cost optimizing. As a stepping stone, the modified Rodrigues Parameters (MRPs) are employed to characterize the relative attitude dynamics. A state transformation method is used to transform the constrained dynamics to an unconstrained dynamics by the log-type function. Then, an ADP algorithm is developed to deal with the Hamilton-Jacobi-Bellman equation of optimal control problem. The convergence and stability are analyzed by the Lyapunov-based method. Finally, the effectiveness of the proposed scheme is demonstrated by numerical simulation.

KW - Adaptive Dynamic Programming (ADP)

KW - Prescribed Performance Control

KW - Reinforcement Learning

KW - Spacecraft Attitude Control

UR - https://www.scopus.com/pages/publications/85125183083

U2 - 10.1109/CCDC52312.2021.9602522

DO - 10.1109/CCDC52312.2021.9602522

M3 - 会议稿件

AN - SCOPUS:85125183083

T3 - Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021

SP - 6121

EP - 6126

BT - Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 33rd Chinese Control and Decision Conference, CCDC 2021

Y2 - 22 May 2021 through 24 May 2021

ER -

Yang H, Fang Y, Guo M, Zhang B, Zhang Y, Hu Q. ADP-Based Prescribed Performance Attitude Tracking Control for Rigid Spacecraft. 在 Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021. Institute of Electrical and Electronics Engineers Inc. 2021. 页码 6121-6126. (Proceedings of the 33rd Chinese Control and Decision Conference, CCDC 2021). doi: 10.1109/CCDC52312.2021.9602522

ADP-Based Prescribed Performance Attitude Tracking Control for Rigid Spacecraft

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