航天器飞轮转子系统的微振动分析、抑制和隔离:综述

Vibration Pub Date : 2024-03-11 DOI:10.3390/vibration7010013
Q. Han, Shuai Gao, Fulei Chu
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引用次数: 0

摘要

本文首先简要介绍了航天器飞轮转子系统(SFRS)微振动的主要激励源,然后从建模方法、抑制手段、隔振技术和地面模拟试验等四个方面系统梳理了相关研究进展。最后,给出了当前研究存在的问题和进一步研究的方向,以更好地服务于现有模型的微振动预测和灵敏度分析,为下一代高精度航天器的微振动抑制和隔振提供参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Micro-Vibration Analysis, Suppression, and Isolation of Spacecraft Flywheel Rotor Systems: A Review
In this paper, the main excitation sources of micro vibration of spacecraft flywheel rotor systems (SFRSs) are briefly described, and then the research progress is systematically reviewed from four perspectives, including modeling methods, suppression means, vibration isolation techniques, and ground simulation tests. Finally, the existing problems of current research and the direction of further research are given to better serve the micro-vibration prediction and sensitivity analysis of existing models, and provide reference points for the micro-vibration suppression and isolation of the next generation of high-precision spacecraft.
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