@inproceedings{bd501ff3cfb24fa29db0783a0ba314a3,
title = "Fuzzy-Logic-Based Integrated Orbit-Attitude-Vibration Prescribed-Time Control for Large-Scale Flexible Spacecraft",
abstract = "This paper investigates a fuzzy-logic-based integrated orbit-attitude-vibration prescribed-time controller for large-scale flexible spacecraft to achieve the high-precision orbit-attitude-vibration stabilization. Due to the existence of nonlinear coupling effects, a refined T-S fuzzy model based on the orbit-attitude-vibration dynamics of large-scale flexible spacecraft is constructed to represent the nonlinear characteristics and avoid the calculation singularity. Then, a prescribed-time controller is designed to stabilize the closed-loop system within a prescribed time with precise convergence rate where Lyapunov stability analysis is performed to prove the prescribed-time stability. Simulation results shows the effectiveness of the proposed control strategy.",
keywords = "Integrated control, Large-scale flexible spacecraft, Prescribed-time control, T-S fuzzy model",
author = "Xiaokui Yue and Bailiang Lyu and Chuang Liu",
note = "Publisher Copyright: {\textcopyright} 2024, The Author(s), under exclusive license to Springer Nature Switzerland AG.; 29th International Conference on Computational and Experimental Engineering and Sciences, ICCES 2023 ; Conference date: 26-05-2023 Through 29-05-2023",
year = "2024",
doi = "10.1007/978-3-031-42987-3\_58",
language = "英语",
isbn = "9783031429866",
series = "Mechanisms and Machine Science",
publisher = "Springer Science and Business Media B.V.",
pages = "839--849",
editor = "Shaofan Li",
booktitle = "Computational and Experimental Simulations in Engineering - Proceedings of ICCES 2023—Volume 2",
}