Yue Yu

Dr. Yue Yu

Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences
+1
orcid

Research Focus & Metrics

Academic Career Length

14Years (2013-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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6 March 2020 in Sensors
Verified
Journal Article
Open access
PDF file
YYYue Yu
Yue Yu
LDLu Dai
Lu Dai
MCMao-Sheng Chen
Mao-Sheng Chen
LKLing-Bo Kong
Ling-Bo Kong
CWChao-Qun Wang
Chao-Qun Wang
ZXZhi-Peng Xue
Zhi-Peng Xue
The accuracy of the circular grating is the key point for control precision of the single gimbal control moment gyroscope servo system used in civilian micro-agile satellites. Instead of using the multi reading heads to eliminate eccentricity errors, an algorithm compensation method based on a calibration experiment using a single reading head was proposed to realize a low-cost and high accuracy angular position measurement. Moreover, the traditional hardware compensation method using double reading heads was also developed for comparison. Firstly, the single gimbal control moment gyroscope system of satellites was introduced. Then, the errors caused by the installation of the reading head were studied and the mathematic models of these errors were developed. In order to construct the compensation function, a calibration experiment using the autocollimator and 24-sided prism was performed. Comparison of angle error compensation using the algorithm and hardware method was presented, and results showed that the algorithm compensation method proposed by this paper achieved the same accuracy level as the hardware method. Finally, the proposed method was further verified through a control system simulation.

1 January 2013 in International Immunopharmacology
Verified
Journal Article
Closed access
LYLiang Yang
Liang Yang
XWXiuli Wu
Xiuli Wu
MWMin Wan
Min Wan
YYYue Yu
Yue Yu
YYYongli Yu
Yongli Yu
LWLiying Wang
Liying Wang

18 August 2022 in PLOS ONE
Verified
Journal Article
Open access
PDF file
YYYue Yu
Yue Yu
LDLu Dai
Lu Dai
MCMaosheng Chen
Maosheng Chen
LKLingbo Kong
Lingbo Kong
CWChaoqun Wang
Chaoqun Wang
ZXZhipeng Xue
Zhipeng Xue
Effective identification of the control model is one of the key aspects in improving the performance of the single gimbal control moment gyroscope (SGCMG) servo system. The accuracy and stability of the servo system can be improved by studying system identification and mechanical resonance frequency. In this study, firstly, the SGCMG gimbal servo system was simplified to a two-mass block model. The theoretical mathematical model of the system’s transfer function and mechanical resonance frequency was derived. Secondly, this paper studied the effective suppression method for mechanical resonance. Thirdly, the mathematical model of the orthogonal correlation analysis method was deduced for system identification. Then, an experimental platform was investigated to obtain the frequency characteristic curve and the transfer function. Finally, the frequency characteristic curve obtained using the transfer function model was plotted and compared with the frequency characteristic curve obtained experimentally. Our results indicate that the orthogonal correlation analysis has a high identification accuracy.