Multimodal Tuning of an Axisymmetric Resonator
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Published:2019-05-02
Issue:9
Volume:141
Page:
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ISSN:0022-0434
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Container-title:Journal of Dynamic Systems, Measurement, and Control
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language:en
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Short-container-title:
Author:
Behbahani Amir H.1, M'Closkey Robert T.2
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of California, Los Angeles, Los Angeles, CA 90095 2. Professor Department of Mechanical and Aerospace Engineering, University of California, Los Angeles, Los Angeles, CA 90095 e-mail:
Abstract
This paper reports an approach for the simultaneous elimination of the modal frequency differences within two pairs of modes in an axisymmetric resonator. Fabricated devices exhibit frequency detuning, which can be eliminated by strategically mass loading the resonator. Each pair of modes responds to the mass loading differently so models are developed to predict the postloading frequency differences. The models are incorporated into a search procedure to select deposition sites that simultaneously reduce the modal frequency difference within each pair. The proposed approach is successfully implemented on a resonator whose modal frequency differences are reduced below 200 mHz from an initial frequency difference of 23.5 Hz for a pair of modes at 13.8 kHz, and a 2.4 Hz difference for another pair of modes at 24.3 kHz.
Publisher
ASME International
Subject
Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering
Reference19 articles.
1. Isolated Planar Gyroscope With Internal Radial Sensing and Actuation,2006 2. Nitzan, S., Ahn, C., Su, T.-H., Li, M., Ng, E., Wang, S., Yang, Z., O'Brien, G., Boser, B., Kenny, T., and Horsley, D., 2013, “Epitaxially-Encapsulated Polysilicon Disk Resonator Gyroscope,” IEEE MEMS, Taipei, Taiwan, Jan. 20–24, pp. 625–628. 3. Kim, D., and M'Closkey, R., 2014, “A MEM Vibratory Gyro With Mode-Matching Achieved by Resonator Mass Loading,” IEEE/ION Position, Location and Navigation Symposium, Monterey, CA, May 5–8, pp. 499–503. 4. Challoner, A., Ge, H., and Liu, J., 2014, “Boeing Disc Resonator Gyroscope,” IEEE/ION Position, Location and Navigation Symposium, Monterey, CA, May 5–8, pp. 504–514. 5. Spectral Analysis of Vibratory Gyro Noise;IEEE Sens. J.,2013
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