@inproceedings{178aeb6f742148b98007160296a34037,
title = "Finite-Time Orbit-Attitude Coupling Control for Flying Around Non-cooperative Targets",
abstract = "In this paper, the attitude and orbit coupling dynamics of the spacecraft is modelled in the sight coordinate, and the joint attitude and orbit controller is designed based on the method of adding a power integral, which can guarantee the finite-time stability of the spacecraft with the expected precision satisfied to fly around non-cooperative targets. It is shown that the proposed algorithm has robustness to the external disturbances. Finally, an numeral example is included to illustrate the effectiveness of the obtained results.",
keywords = "Adding A Power Integral Method, Finite-time Control, Fly-around, Non-cooperative Targets",
author = "Yiwei Tang and Yingmin Jia",
note = "Publisher Copyright: {\textcopyright} 2022 Technical Committee on Control Theory, Chinese Association of Automation.; 41st Chinese Control Conference, CCC 2022 ; Conference date: 25-07-2022 Through 27-07-2022",
year = "2022",
doi = "10.23919/CCC55666.2022.9902403",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "3299--3304",
editor = "Zhijun Li and Jian Sun",
booktitle = "Proceedings of the 41st Chinese Control Conference, CCC 2022",
address = "美国",
}