0.0062\ ^/\sqrt Angle Random Walk and 0.027\ ^/hr Bias Instability from a Micro-Shell Resonator Gyroscope with Surface Electrodes
This paper reports measured results for a fused-silica precision shell integrating (PSI) micro gyroscope employing out-of-plane drive/sense transduction mechanism. The PSI gyroscope is made with a 5 mm radius shell resonator operating in n=2 wine-glass mode at a frequency ( f_{n=2} ) of 5.803 kHz wi...
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Published in | 2020 IEEE 33rd International Conference on Micro Electro Mechanical Systems (MEMS) pp. 737 - 740 |
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Main Authors | , , , , |
Format | Conference Proceeding |
Language | English |
Published |
IEEE
01.01.2020
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Subjects | |
Online Access | Get full text |
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Summary: | This paper reports measured results for a fused-silica precision shell integrating (PSI) micro gyroscope employing out-of-plane drive/sense transduction mechanism. The PSI gyroscope is made with a 5 mm radius shell resonator operating in n=2 wine-glass mode at a frequency ( f_{n=2} ) of 5.803 kHz with as-fabricated frequency split ( \Delta f ) of 2.1 Hz. Large and reasonably uniform capacitance (∼0.25 pF) is achieved with flat surface electrodes. The gyroscope is operated in the force-rebalance mode by interfacing with an ultra-low-noise transimpedance amplifier (TIA). Near-navigation grade angle random walk (ARW) of 0.0062\ \deg/\sqrt{\mathrm{h}}\mathrm{r} , in-run bias instability (BI) of 0.027 deg/hr and scale factor of 158 mV/deg/s without any temperature compensation are achieved. |
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ISSN: | 2160-1968 |
DOI: | 10.1109/MEMS46641.2020.9056391 |