IP Library Granted Patent US 8,210,023
Granted Patent B2
US 8,210,023 · App. 12/520,335 · Granted Jul 3, 2012

Method for calibrating a scale factor in an axisymmetrical vibrating gyrometer

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Quick Facts
Patent No.
US 8,210,023
App. No.
12/520,335
Granted
Jul 3, 2012
Kind
B2
Abstract

The method of calibrating a scale factor of an axially-symmetrical vibrating rate gyro operating by applying an amplitude control signal (CA) and a precession control signal (CP) to a vibrator member ( 1 ) set into vibration at a given frequency comprises a pre-calibration step consisting in calculating a reference gain ratio between a drive gain (Gmx) in a first direction and a drive gain (Gmy) in a second direction in modal quadrature with the first direction, and in storing the reference gain ratio, and a calibration step consisting in calculating a value for a measurable magnitude associated with the scale factor by a proportionality relationship including the reference gain ratio, and calculating a corrected scale factor on the basis of the value of the measurable magnitude and the stored reference gain ratio.

Claims (6)

1. A method of calibrating a scale factor of an axially-symmetrical vibrating rate gyro operating by applying an amplitude control signal (CA) and a precession control signal (CP) to a vibrator member set into vibration at a given frequency, wherein the method comprises a pre-calibration step consisting in calculating a reference gain ratio between a drive gain (Gmx) in a first direction and a drive gain (Gmy) in a second direction in modal quadrature with the first direction, and in storing the reference gain ratio, and a calibration step consisting in calculating a value for a measurable magnitude associated with the scale factor by a proportionality relationship including the reference gain ratio, and calculating a corrected scale factor on the basis of the value of the measurable magnitude and the stored reference gain ratio.

2. A calibration method according to claim 1 , wherein the measurable magnitude is a variation in the vibration frequency as a function of a variation in a stiffness control signal applied to at least one control electrode.

3. A calibration method according to claim 2 , wherein the stiffness control signal is in time quadrature with the amplitude control signal and the precession control signal, and the stiffness control signal is in modal quadrature geometrically with the precession control signal.

4. A calibration method according to claim 1 , wherein the measurable magnitude is an amplitude variation as a function of a variation in the amplitude control signal (CA).

5. A calibration method according to claim 4 , wherein the amplitude control signal (CA) is generated to cause a variation in amplitude away from a setpoint amplitude (Ac) to a low amplitude threshold, followed by an inverse variation from the low amplitude threshold up to the setpoint amplitude (Ac).

6. A calibration method according to claim 5 , wherein the low amplitude threshold is equal to half the setpoint amplitude.

Assignments (2)
CHANGE OF NAME Recorded May 6, 2018
From: SAGEM DÉFENSE SÉCURITÉ
To: SAFRAN ELECTRONICS & DEFENSE
Reel/Frame 046082/0606 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 19, 2009
From: JEANROY, ALAIN; RENAULT, ALAIN; CARON, JEAN-MICHEL
To: SAGEM DEFENSE SECURITE
Reel/Frame 022858/0675 →