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 :
بازگشت