@inproceedings{3ec258a8d8eb46159e40bdc3c3c58437,
title = "Adaptive Robust Control for Flexible Spacecraft with LQR Vibration Suppression",
abstract = "This paper presents a combined strategy of the attitude control and vibration suppression for spacecraft with flexible appendages, in the presence of inertia parameter uncertainties and external disturbances. An adaptive robust output feedback controller is designed to achieve precise attitude control under parametric uncertainties and disturbances, and a LQR controller is proposed to suppress residual vibration. The effectiveness of the proposed method is verified by theorem proof and simulation results.",
keywords = "Adaptive Control, Flexible Spacecraft, Linear Quadratic Regulator, Robust Control",
author = "Zhen Chen and Jing Du and Xiangdong Liu and Pingli Lu",
note = "Publisher Copyright: {\textcopyright} 2020 Technical Committee on Control Theory, Chinese Association of Automation.; 39th Chinese Control Conference, CCC 2020 ; Conference date: 27-07-2020 Through 29-07-2020",
year = "2020",
month = jul,
doi = "10.23919/CCC50068.2020.9189603",
language = "English",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "6978--6983",
editor = "Jun Fu and Jian Sun",
booktitle = "Proceedings of the 39th Chinese Control Conference, CCC 2020",
address = "United States",
}