Method for compensation for a zero error in a coriolis gyro

Measuring and testing – Instrument proving or calibrating – Angle – direction – or inclination

Reexamination Certificate

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Reexamination Certificate

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10553110

ABSTRACT:
A method for compensation of the zero error of a Coriolis gyro. The frequency of the read oscillation is modulated. The output signal from a rotation rate control loop or quadrature control loop for the Coriolis gyro is demodulated in synchronism with the modulation of the frequency of the read oscillation to obtain an auxiliary signal. The auxiliary signal is a measure of the zero error. A compensation signal is produced and passed to the input of the rotation rate control loop or quadrature control loop, with the compensation signal being controlled such that the magnitude of the auxiliary signal is as small as possible.

REFERENCES:
patent: 5908986 (1999-06-01), Mitamura
patent: 6205838 (2001-03-01), Schmid et al.
patent: 19845185 (2000-04-01), None
patent: 19939998 (2001-03-01), None
patent: 19910415 (2001-09-01), None
patent: 10062347 (2002-06-01), None
patent: 69615468 (1997-01-01), None
patent: 0114831 (2001-03-01), None

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