@inproceedings{155aeb6154f8488e9ef6d35aad41fe87,
title = "ICM-based experimental identification of couple unbalance for GyroWheel system",
abstract = "GyroWheel is an innovative aerospace device which integrates the function of attitude determination and control. Due to the special structure of flex-gimbal suspension system, GyroWheel rotor have three degrees of freedom. As most other rotating machineries, the dynamic unbalance issue also exists in GyroWheel system, which is caused by the uneven mass distribution of rotor. The couple unbalance leads to tilt vibration and induces interference in system operation, especially considering the tilt motion of GyroWheel rotor along radial direction. In this paper, the identification issue of couple unbalance for GyroWheel rotor is investigated by using the ICM-based identification algorithm. The effectiveness and feasibility of the identification algorithm is verified according to the experimental results based on the GyroWheel prototype.",
keywords = "Couple unbalance, FFT, GyroWheel, Influence coefficient method",
author = "Haiyuan Liu and Xin Huo and Zhaosheng Guo and Sizhao Feng and Yongjiang Pi and Yu Yao",
note = "Publisher Copyright: {\textcopyright} 2017 Technical Committee on Control Theory, CAA.; 36th Chinese Control Conference, CCC 2017 ; Conference date: 26-07-2017 Through 28-07-2017",
year = "2017",
month = sep,
day = "7",
doi = "10.23919/ChiCC.2017.8027701",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "2305--2309",
editor = "Tao Liu and Qianchuan Zhao",
booktitle = "Proceedings of the 36th Chinese Control Conference, CCC 2017",
address = "美国",
}