@inproceedings{31cacfa64b9e4b629337ac84ac361044,
title = "Finite-Time Control for Combination Spacecraft Attitude Based on LESO of Auxiliary System",
abstract = "This paper proposes a finite-time control method for the attitude of combined spacecraft without system parameter identification, avoiding the problems of long identification time and low identification accuracy of the combined spacecraft parameters. The method designs an auxiliary system based on the features of the model, combines the Linear Extended State Observer (LESO) and non-singular terminal sliding mode control(SMC), and achieves the finite-time attitude control of the combined spacecraft.",
keywords = "Combined spacecraft, Finite-time control, LESO, Non-singular terminal SMC",
author = "Xiao Han and Lifan Zhou and Guangfu Ma and Xixuan Chen",
note = "Publisher Copyright: {\textcopyright} 2023, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.; International Conference on Guidance, Navigation and Control, ICGNC 2022 ; Conference date: 05-08-2022 Through 07-08-2022",
year = "2023",
doi = "10.1007/978-981-19-6613-2\_670",
language = "英语",
isbn = "9789811966125",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "6955--6965",
editor = "Liang Yan and Haibin Duan and Yimin Deng and Liang Yan",
booktitle = "Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control",
address = "德国",
}