DocumentCode
2961500
Title
Phase research of no-drive structure silicon micromachined gyroscope
Author
Xu, X.S. ; Liu, H.L. ; Zhang, F.X.
Author_Institution
Res. Centre of Sensor Technol., Beijing Inf. Sci. & Technol. Univ., Beijing
fYear
2008
fDate
5-8 Aug. 2008
Firstpage
939
Lastpage
942
Abstract
The phase picking up technique of silicon micromachined gyroscope used for rotating carrier is introduced. When the sensitivity axis is parallel to the deflexion plane, silicon pendulum will get the biggest Coriolis force, and the outputs are the peak value of the sine wave. However, when the sensitivity axis is perpendicularity to the deflexion plane, the outputs are the zero value of the sine wave. The self-rotated signal of the carrier (accelerometer) as benchmark, comparing to the output signal phase of the carrier and the gyroscope, then subtract the lagged value from the phase difference of the accelerometer and the gyroscope, we can confirm the real deflecting direction of the carrier in the space.
Keywords
Coriolis force; gyroscopes; micromachining; micromechanical devices; sensitivity analysis; Coriolis force; deflexion plane; no-drive structure silicon micromachined gyroscope; rotating carrier; sensitivity axis; silicon pendulum; Accelerometers; Angular velocity; Ceramics; Gas detectors; Gyroscopes; Information science; Signal processing; Silicon; Space technology; Structural beams;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2008. ICMA 2008. IEEE International Conference on
Conference_Location
Takamatsu
Print_ISBN
978-1-4244-2631-7
Electronic_ISBN
978-1-4244-2632-4
Type
conf
DOI
10.1109/ICMA.2008.4798884
Filename
4798884
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