@inproceedings{4fd6e788767a4897be385a3a89670f41,
title = "Attitude Control of Fully-Actuated Flexible Spacecraft Based on Linear Active Disturbance Rejection Control",
abstract = "A method for controlling a spacecraft's attitude and reducing vibrations is proposed, which involves utilizing linear active disturbance rejection control (LADRC) for precise tracking and vibration suppression. This method utilizes a dynamic model based on the finite element method and ensures the system is fully controllable. To enhance stability and practicality, an ADRC controller is designed for the system. An extended state observer is used to estimate and compensate for disturbances, resulting in effective attitude tracking and vibration suppression. The theoretical derivation and simulation analysis confirm that the closed-loop system exhibits uniform ultimate stability. Theoretical analysis and simulation results validate the efficacy of the proposed approach in achieving attitude control and vibration suppression.",
keywords = "ADRC, Extended state observer, Flexible spacecraft, Fully actuated model, Stable",
author = "Yudong Hu and Zhongwei Shi and Xu Li and Yuxuan Chen and Changsheng Gao",
note = "Publisher Copyright: {\textcopyright} The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2025.; International Conference on Guidance, Navigation and Control, ICGNC 2024 ; Conference date: 09-08-2024 Through 11-08-2024",
year = "2025",
doi = "10.1007/978-981-96-2212-2\_25",
language = "英语",
isbn = "9789819622115",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "249--257",
editor = "Liang Yan and Haibin Duan and Yimin Deng",
booktitle = "Advances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 4",
address = "德国",
}