Resonator fiber optic gyroscope resonance detection demodulator reference phase corrector

Patent metadata

Field	Value
Publication number	US-9683846-B2
Application number	US-201514949552-A
Country	US
Kind code	B2
Filing date	Nov 23, 2015
Priority date	Nov 23, 2015
Publication date	Jun 20, 2017
Grant date	Jun 20, 2017

Abstract

A RFOG, comprising: a master laser emitting a reference optical signal; first and second slave lasers emitting first and second optical signals; an optical resonator ring cavity coupled to the lasers, the first and second optical signals propagating in first and second directions through the optical resonator ring cavity; one or more signal generators to inject first and second modulation signals at first and second frequencies on both optical signals; first and second photodetectors that generate first and second signals; first and second demodulators to demodulate the first and second signals using first and second reference signals and the first and second frequencies; a differencing function to output the difference between resonance frequencies of the first and second signals; at least a third demodulator to detect reference phase errors; and at least one phase servo to adjust the phase of at least one of the first and second reference signals.

First claim

What is claimed is:

1. A resonator fiber optic gyroscope (RFOG), comprising:
a master laser configured to emit a reference optical signal;
a first slave laser configured to emit a first optical signal;
a second slave laser configured to emit a second optical signal;
an optical resonator ring cavity coupled to the master laser, first slave laser, and second slave laser, wherein the first optical signal propagates in a first direction through the optical resonator ring cavity, and the second optical signal propagates in a second direction through the optical resonator ring cavity;
one or more signal generators configured to inject a first modulation signal at a first frequency and second modulation signal at a second frequency on both the first optical signal and the second optical signal;
a first photodetector that generates a first signal corresponding to the first optical signal based on a signal exiting the optical resonator ring cavity at a first transmission port;
a second photodetector that generates a second signal corresponding to the second optical signal based on a signal exiting the optical resonator ring cavity at a second transmission port;
a first demodulator configured to demodulate the first signal in phase with a first reference signal and at the first frequency to produce a first demodulated signal;
a second demodulator configured to demodulate the second signal in phase with a second reference signal and at the first frequency to produce a second demodulated signal, wherein the first reference signal and the second reference signal are derived from the first modulation signal;
a differencing function configured to output the difference between resonance frequencies of the first signal and the second signal based on the first demodulated signal and the second demodulated signal;
at least a third demodulator configured to detect a reference phase error; and
at least one phase servo electronics module configured to adjust the phase of at least one of the first reference signal and the second reference signal based on the detected reference phase error.

2. The RFOG of claim 1 , further comprising first optical phase lock loop (OPLL) electronics coupled to the first slave laser and second OPLL electronics coupled to the second slave laser, wherein the first slave laser is phase-locked to the master laser using the first OPLL electronics and the second slave laser is phase-locked to the master laser using the second OPLL electronics.

3. The RFOG of claim 2 , further comprising:
a first servo electronics module coupled to the first demodulator, wherein the first servo electronics module controls an output of a first direct digital synthesizer (DDS) that provides a local oscillator signal for the first OPLL electronics; and
a second servo electronics module coupled to the second demodulator, wherein the second servo electronics module controls an output of a second DDS that provides a local oscillator signal for the second OPLL electronics.

4. The RFOG of claim 3 , further comprising:
a third photodetector coupled to a reflection port of the resonator; and
Pound-Drever-Hall (PDH) electronics coupled to the third photodetector and the master laser, wherein the PDH electronics receive the second modulation signal, wherein the second modulation signal comprises a PDH set-point modulation signal, wherein the PDH electronics applies the PDH set-point modulation signal to the reference optical signal, wherein the PDH set-point modulation signal modulates the reference optical signal at the second frequency.

5. The RFOG of claim 4 , wherein the second frequency is outside of a measurement band of the RFOG.

6. The RFOG of claim 4 , wherein the first demodulator is a dual-phase demodulator having an in-phase output and a quadrature output, wherein the second demodulator is a dual-phase demodulator having an in-phase output and a quadrature output.

7. The RFOG of claim 6 , wherein the at least a third demodulator comprises:
a third demodulator configured to demodulate a quadrature signal from the quadrature output of the first demodulator at the second frequency to produce a third demodulated signal, wherein the third demodulated signal corresponds to a phase error of the first reference signal; and
a fourth demodulator configured to demodulate a quadrature signal from the quadrature output of second demodulator at the second frequency to produce a fourth demodulated signal, wherein the fourth demodulated signal corresponds to a phase error of the second reference signal;
wherein the at least one phase servo electronics module comprises:
a first phase servo electronics module coupled to the third demodulator, wherein the first phase servo electronics module adjusts the phase of the first reference signal to drive the third demodulated signal toward zero; and
a second phase servo electronics module coupled to the fourth demodulator, wherein the second phase servo electronics module adjusts the phase of the second reference signal to drive the fourth demodulated signal toward zero.

8. The RFOG of claim 3 , wherein the second modulation signal comprises a second harmonic frequency of the first modulation signal plus a delta-f frequency, wherein the second modulation signal is summed with the first modulation signal prior to being injected on the first optical signal and the second optical signal.

9. The RFOG of claim 8 , further comprising a mixer configured to multiply the first modulation signal with the second modulation signal to produce a third reference signal at the delta-f frequency;
wherein the at least a third demodulator comprises a third demodulator configured to demodulate a signal output from the differencing function in phase with the third reference signal and at the delta-f frequency to produce a third demodulated signal, wherein the third demodulated signal corresponds to a phase error of the first reference signal; and
wherein the at least one phase servo electronics module comprises a first phase servo electronics module coupled to the third demodulator, wherein the first phase servo electronics module adjusts the phase of the first reference signal to drive the third demodulated signal toward zero.

10. The RFOG of claim 8 , further comprising a mixer configured to multiply the first modulation signal and the second modulation signal to produce a third reference signal at the delta-f frequency;
wherein the at least a third demodulator comprises:
a third demodulator configured to demodulate the first demodulated signal in phase with the third reference signal and at the delta-f frequency to produce a third demodulated signal, wherein the third demodulated signal corresponds to a phase error of the first reference signal; and
a fourth demodulator configured to demodulate the second demodulated signal in phase with the third reference signal and at the delta-f frequency to produce a fourth demodulated signal, wherein the fourth demodulated signal corresponds to a phase error of the second reference signal;

wherein the at least one phase servo electronics module comprises:
a first phase servo electronics module coupled to the third demodulator, wherein the first phase servo electronics module adjusts the phase of the first reference signal to drive the third demodulated signal toward zero; and
a second phase servo electronics module coupled to the fourth demodulator, wherein the second phase servo electronics module adjusts the phase of the second reference signal to drive the fourth demodulated signal toward zero.

11. A method of reducing common modulation errors for a resonator fiber optic gyroscope (RFOG) during operation, comprising:
injecting a f

Assignees

• Honeywell Int Inc

Inventors

• Strandjord Lee K
• Ho Waymon
• Croker Chuck

Classifications

• G01C19/727 Primary

  using a passive ring resonator · CPC title

• G01C19/721

  Details, e.g. optical or electronical details · CPC title

• G01C19/726 Primary

  Phase nulling gyrometers, i.e. compensating the Sagnac phase shift in a closed loop system · CPC title