DocumentCode
3422278
Title
The resonating star gyroscope
Author
Zaman, M.F. ; Sharma, A. ; Amini, B.V. ; Ayazi, F.
Author_Institution
Integrated MEMS Lab., Georgia Inst. of Technol., Atlanta, GA, USA
fYear
2005
fDate
30 Jan.-3 Feb. 2005
Firstpage
355
Lastpage
358
Abstract
This paper introduces the resonating star gyroscope (RSG), a new vibratory shell-type structure for rate sensing. The structure formed as a merged superposition of two square shells, yields in-plane degenerate flexural modes that are used to sense z-axis rotation. A high aspect ratio polysilicon implementation utilizing the primary degenerate flexural modes of the gyroscope exhibits an open-loop rate sensitivity of 1.6mV/°/s. The Brownian noise floor of the sensor with a quality factor (Q) of 1500 and drive amplitude of 100nm is 0.03°/s/√Hz. The RSG may also function at higher-order flexural modes. A single crystal silicon design explores such an operation. Preliminary characterization results yield matched-mode operation and very high-Q higher-order degenerate flexural modes (Q∼100k).
Keywords
Q-factor; gyroscopes; microsensors; Brownian noise floor; drive amplitude; high aspect ratio polysilicon implementation; in-plane degenerate flexural modes; matched-mode operation; open-loop rate sensitivity; quality factor; rate sensing; resonating star gyroscope; single crystal silicon design; vibratory shell-type structure; z-axis rotation sensing; Electrodes; Etching; Fabrication; Flexible manufacturing systems; Gyroscopes; Hafnium; Resonance; Resonant frequency; Shape; Springs;
fLanguage
English
Publisher
ieee
Conference_Titel
Micro Electro Mechanical Systems, 2005. MEMS 2005. 18th IEEE International Conference on
ISSN
1084-6999
Print_ISBN
0-7803-8732-5
Type
conf
DOI
10.1109/MEMSYS.2005.1453940
Filename
1453940
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