Appointed-time attitude-orbit coupling control for distributed spacecraft formation

被引：0
|
作者：
Liu Y. [1 ]
Cao L. [2 ]
Qin K.-Y. [1 ]
Xiao B. [3 ]
Shi M.-J. [1 ]
Li W.-H. [1 ]
机构：
[1] School of Aeronautics and Astronautics, University of Electronic Science and Technology of China, Sichuan, Chengdu
[2] National Innovation Institute of Defense Technology, Chinese Academy of Military Science, Beijing
[3] School of Automation, Northwestern Polytechnical University, Shaanxi, Xi’an
来源：
Kongzhi Lilun Yu Yingyong/Control Theory and Applications | 2024年 / 41卷 / 05期
基金：
中国国家自然科学基金;
关键词：
appointed-time control; attitude and orbit coupled control; prescribed performance control; spacecraft formation flying; spacecraft formation reconfiguration;
D O I：
10.7641/CTA.2023.20595
中图分类号：
学科分类号：
摘要：
This paper addresses the problem of appointed-time attitude and orbit coupled control for distributed spacecraft formation with parameter uncertainties, external disturbances and requirements of prescribed performance. A low complexity cooperative controller was proposed based on the prescribed performance control method, which realized the spacecraft formation flying within the set time and the formation errors met the preset performance indexes. Firstly, an appointed-time performance function that can arbitrarily set the stability time of the system is introduced by using the concept of finite time stability. Secondly, by combining the appointed-time performance function with the prescribed performance control method, a appointed-time cooperative controller is designed to ensure the transient performance and the steady performance and finite-time stability of spacecraft formation control system. And the controller is independent of spacecraft mass and moment of inertia. Finally, the Lyapunov stability theorem is applied to prove the stability of the control system, and numerical simulation results show the effectiveness of the control law. © 2024 South China University of Technology. All rights reserved.
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页码：829 / 838
页数：9
相关论文
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