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Dual-mass vibratory rate gyroscope with suppressed translational acceleration response and quadrature-error correction capabilityA microfabricated vibratory rate gyroscope to measure rotation includes two proof-masses mounted in a suspension system anchored to a substrate. The suspension has two principal modes of compliance, one of which is driven into oscillation. The driven oscillation combined with rotation of the substrate about an axis perpendicular to the substrate results in Coriolis acceleration along the other mode of compliance, the sense-mode. The sense-mode is designed to respond to Coriolis accelerationwhile suppressing the response to translational acceleration. This is accomplished using one or more rigid levers connecting the two proof-masses. The lever allows the proof-masses to move in opposite directions in response to Coriolis acceleration. The invention includes a means for canceling errors, termed quadrature error, due to imperfections in implementation of the sensor. Quadrature-error cancellation utilizes electrostatic forces to cancel out undesired sense-axis motion in phase with drive-mode position.
Document ID
20080004510
Acquisition Source
Goddard Space Flight Center
Document Type
Other - Patent
Authors
Clark, William A.
Juneau, Thor N.
Lemkin, Mark A.
Roessig, Allen W.
Date Acquired
August 24, 2013
Publication Date
May 15, 2001
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Number: US-PATENT-6,230,563
Patent Application Number: US-PATENT-APPL-SN-321972
Funding Number(s)
CONTRACT_GRANT: NAS5-97227
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-6,230,563
Patent Application
US-PATENT-APPL-SN-321972
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