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contributor authorDavid Schwartz
contributor authorRobert T. M’Closkey
date accessioned2017-05-09T00:49:12Z
date available2017-05-09T00:49:12Z
date copyrightMarch, 2012
date issued2012
identifier issn0022-0434
identifier otherJDSMAA-26582#021005_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148506
description abstractAxisymmetric 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleDecoupling of a Disk Resonator From Linear Acceleration Via Mass Matrix Perturbation
typeJournal Paper
journal volume134
journal issue2
journal titleJournal of Dynamic Systems, Measurement, and Control
identifier doi10.1115/1.4005275
journal fristpage21005
identifier eissn1528-9028
keywordsSensors
keywordsMagnets
keywordsDisks
keywordsApproximation
keywordsAccelerometers
keywordsCenter of mass
keywordsOptimization
keywordsStiffness
keywordsFrequency response
keywordsFrequency
keywordsSignals AND Measurement
treeJournal of Dynamic Systems, Measurement, and Control:;2012:;volume( 134 ):;issue: 002
contenttypeFulltext


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