DocumentCode
1289296
Title
Integrated Model and Compensation of Thermal Errors of Silicon Microelectromechanical Gyroscope
Author
Jiancheng, Fang ; Jianli, Li
Author_Institution
Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
Volume
58
Issue
9
fYear
2009
Firstpage
2923
Lastpage
2930
Abstract
Based on the thermal interferential moment, the dynamic thermal error induced by accelerations of a microelectromechanical system (MEMS) gyroscope is analyzed. The electromechanical-thermal error is discussed. The integrated thermal error compensation method considering the electromechanical-thermal error and the dynamic thermal error induced by accelerations is proposed. The experimental results show that the bias temperature sensitivity is reduced by more than one order of magnitude compared with the raw bias temperature sensitivity of the gyroscope. The integrated compensation method is reasonable and effective in the temperature error compensation of the MEMS gyroscope and outperforms the classical compensation method in performance.
Keywords
error analysis; error compensation; gyroscopes; microsensors; silicon; thermal analysis; MEMS gyroscope; Si; aerospace system; bias temperature sensitivity; classical compensation method; dynamic thermal error; electromechanical-thermal error; error analysis; integrated thermal error compensation method; microelectromechanical system; silicon microelectromechanical gyroscope; temperature error compensation; thermal interferential moment; Error analysis; error compensation; gyroscope; microelectromechanical devices; temperature;
fLanguage
English
Journal_Title
Instrumentation and Measurement, IEEE Transactions on
Publisher
ieee
ISSN
0018-9456
Type
jour
DOI
10.1109/TIM.2009.2016780
Filename
5196812
Link To Document