DocumentCode
1857949
Title
Design trade-offs of micromachined gyroscope concept allowing interchangeable operation in both robust and precision modes
Author
Schofield, A.R. ; Trusov, A.A. ; Shkel, A.M.
Author_Institution
Dept. of Mech. & Aerosp. Eng., Univ. of California, Irvine, CA, USA
fYear
2009
fDate
21-25 June 2009
Firstpage
1952
Lastpage
1955
Abstract
This paper presents design trade-offs for a z-axis gyroscope allowing interchangeable operation in either precision or robust modes. This is enabled through a complete 2-DOF sense mode which allows the specification of the peak spacing and degree of coupling independent of frequency. Simulated sense mode frequency responses for various coupling amounts indicate that weakly coupled systems are desirable due to the larger precision mode gain increase (over 20 dB) for atmospheric pressure operation. Experimentally measured sense mode frequency responses for strong and weak coupling confirm the simulation results in air while also revealing that strong coupling is desirable at vacuum due to the increased precision mode gain improvement of over 40 dB while leaving the robust mode relatively unaffected.
Keywords
frequency response; gyroscopes; micromechanical devices; atmospheric pressure operation; micromachined gyroscope; sense mode frequency responses; z-axis gyroscope; Atmospheric modeling; Bandwidth; Costs; Equations; Gyroscopes; Laboratories; Resonant frequency; Robustness; Suspensions; Vehicle dynamics; Mode-matching; Robustness; Vibratory gyroscope;
fLanguage
English
Publisher
ieee
Conference_Titel
Solid-State Sensors, Actuators and Microsystems Conference, 2009. TRANSDUCERS 2009. International
Conference_Location
Denver, CO
Print_ISBN
978-1-4244-4190-7
Electronic_ISBN
978-1-4244-4193-8
Type
conf
DOI
10.1109/SENSOR.2009.5285672
Filename
5285672
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