@inproceedings{ab746b80d7f9430cbdc4ff97739be447,
title = "Adaptive Finite-time Orbit Control for Spacecraft Formation with External Disturbances",
abstract = "This paper addresses the finite-time orbit control problem for spacecraft formation flying with external disturbances. A new finite-time tracking control strategy with adaptation law and the adding one power integrator method is designed to ensure that the closed-loop system is practical finite-time stable and that the tracking errors of relative position and velocity are bounded within finite-time despite with external disturbances. Finally, an example is shown to validate the effectiveness of the proposed finite-time tracking controller.",
keywords = "Finte-time Control, Spacecraft Formation Flying, backstepping method",
author = "Ruixia Liu and Lei Xing and Yang Yang and Jian Zhang",
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/CCC55666.2022.9901865",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "329--333",
editor = "Zhijun Li and Jian Sun",
booktitle = "Proceedings of the 41st Chinese Control Conference, CCC 2022",
address = "美国",
}