- Patent Title: Gyro quadrature stabalization with demodulation phase error nulling
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Application No.: US14147260Application Date: 2014-01-03
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Publication No.: US09605964B2Publication Date: 2017-03-28
- Inventor: Howard H. Ge , Anthony Dorian Challoner
- Applicant: The Boeing Company
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Agency: Moore & Van Allen PLLC
- Agent Charles L. Moore
- Main IPC: G01C19/00
- IPC: G01C19/00 ; G01C19/5684 ; G01C19/5776

Abstract:
A gyroscope system may include a disc resonator gyroscope including a plurality of electrodes embedded in the disc resonator gyroscope. The electrodes may be configured for at least applying a drive voltage and a tuning voltage to the disc resonator gyroscope and for sensing operating parameters of the disc resonator gyroscope. The gyroscope system may also include a quadrature stabilization circuit configured to measure a quadrature error and generate a quadrature regulating voltage based on the quadrature error. The tuning voltage may be adjusted by the quadrature regulating voltage to cancel an effect of voltage flicker before being applied to a tuning electrode of the disc resonator gyroscope.
Public/Granted literature
- US20150192415A1 GYRO QUADRATURE STABALIZATION WITH DEMODULATION PHASE ERROR NULLING Public/Granted day:2015-07-09
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