Axisymmetric microelectromechanical (MEM) vibratory rate gyroscopes are designed so the central post which attaches the resonator to the sensor case is a nodal point of the two Coriolis-coupled modes that are exploited for angular rate sensing. This configuration eliminates any coupling of linear acceleration to these modes. When the gyro resonators are fabricated, however, small mass and stiffness asymmetries cause coupling of these modes to linear acceleration of the sensor case. In a resonator postfabrication step, this coupling can be reduced by altering the mass distribution on the resonator so that its center of mass is stationary while the operational modes vibrate. In this paper, a scale model of the disk resonator gyroscope (DRG) is used to develop and test methods that significantly reduce linear acceleration coupling.
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e-mail: daves@ucla.edu
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March 2012
Research Papers
Decoupling of a Disk Resonator From Linear Acceleration Via Mass Matrix Perturbation
David Schwartz,
David Schwartz
Postdoctoral Scholar
e-mail: Department of Mechanical and Aerospace Engineering,
e-mail: daves@ucla.edu
University of California
, Los Angeles
, CA 90095
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Robert T. M’Closkey
Robert T. M’Closkey
Professor
e-mail: Department of Mechanical and Aerospace Engineering,
University of California
, Los Angeles
, CA 90095
Search for other works by this author on:
David Schwartz
Postdoctoral Scholar
e-mail: Department of Mechanical and Aerospace Engineering,
University of California
, Los Angeles
, CA 90095e-mail: daves@ucla.edu
Robert T. M’Closkey
Professor
e-mail: Department of Mechanical and Aerospace Engineering,
University of California
, Los Angeles
, CA 90095J. Dyn. Sys., Meas., Control. Mar 2012, 134(2): 021005 (10 pages)
Published Online: December 29, 2011
Article history
Received:
May 26, 2010
Revised:
August 9, 2011
Online:
December 29, 2011
Published:
December 29, 2011
Citation
Schwartz, D., and M’Closkey, R. T. (December 29, 2011). "Decoupling of a Disk Resonator From Linear Acceleration Via Mass Matrix Perturbation." ASME. J. Dyn. Sys., Meas., Control. March 2012; 134(2): 021005. https://doi.org/10.1115/1.4005275
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