IP Library Granted Patent US 7,327,461
Granted Patent B2
US 7,327,461 · App. 11/104,557 · Granted Feb 5, 2008

Method of controlling a laser gyro by the amplitude of the winking signal

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,327,461
App. No.
11/104,557
Granted
Feb 5, 2008
Kind
B2
Abstract

A push-pull method of controlling a laser gyro. At least three mirrors form a closed-loop light path for two laser beams propagating in opposite directions, which is subjected to movement. At least two of the mirrors are associated with actuators connected to push-pull control members for controlling the positions of the mirrors to minimize the amplitude of the winking signal which occurs in a lased intensity signal of the laser beams. The method includes detecting the frequency of the winking signal of at least one laser beam, and of triggering the measurement of the amplitude of the winking signal when the frequency of the winking signal is less than a predetermined threshold corresponding to passing into a dead band of the gyro.

Claims (19)

1. A push-pull method of controlling a laser gyro comprising:

providing at least three mirrors for implementing a closed loop light path for two laser beams propagating in opposite directions,

subjecting the gyro also to dither movement,

providing actuators which are associated with at least two mirrors, said actuators being connected to push-pull control members for controlling the positions of the mirrors so as to minimize the amplitude of a winking signal occurring in a lased intensity signal of the laser beams,

measuring a frequency of the winking signal of at least one laser beam,

triggering measurement of an amplitude of the winking signal when the measured frequency of the winking signal is less than a predetermined threshold corresponding to passing into a dead band of the gyro, and

controlling said actuators through said push-pull control members through the measurement of the amplitude of the winking signal.

2. A method according to claim 1 , further comprising:

providing the gyro with an interferometer receiving the laser beams and generating therefrom an interference signal comprising two fringe signals that are substantially in quadrature, and

filtering at least one fringe signal with high-pass filtering, and

comparing an amplitude of the filtered signal with the predetermined threshold corresponding to passing into the dead band, to trigger said measurement of the amplitude of the winking signal when the filtered signal is less than the predetermined threshold.

3. A method according to claim 2 , further comprising rectifying the filtered signal before the step of comparison with the predetermined threshold.

4. A method according to claim 3 , further comprising filtering the two fringe signals, rectifying the resulting signal, and adding the rectified signal to produce a sum signal prior to performing a comparison with the predetermined threshold.

5. A method according to claim 4 , further comprising smoothing the sum signal by low-pass filtering prior to being compared with the predetermined threshold.

6. A method according to claim 2 , further comprising modulating the predetermined threshold as a function of the amplitude of one of the fringe signals.

7. A method according to claim 2 , the step of measuring the amplitude of the winking signal includes sampling the winking signal extracted from a lased intensity of one of the laser beams.

8. A method according to claim 7 the step of measuring the amplitude of the winking signal includes taking measurements on a plurality of dead-bang crossings, calculating the amplitude of the winking signal based on the measurements of the dead-bang crossing, and providing an output to control the push-pull control members.

9. A method according to claim 1 wherein an entry speed of the gyro is less than or equal to 0.8 times a maximum speed for the dither movement.

10. A method according to claim 1 , further comprising controlling the push-pull control by applying to one mirror actuator a signal representative of the sum of a path length control and a winking adjustment control, and by applying to another mirror actuator a signal representative of a difference between the path length control and the winking adjustment control.

Assignments (3)
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 11, 2008
From: SAGEM SA
To: SAGEM DEFENSE SECURITE
Reel/Frame 021080/0602 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 13, 2005
From: LIGNON, CHRISTIAN
To: SAGEM SA
Reel/Frame 016473/0299 →