System and method for enhancing signal-to-noise ratio of a resonator fiber optic gyroscope

• US 8,223,341 B2
• Filed: 05/28/2010
• Issued: 07/17/2012
• Est. Priority Date: 05/28/2010
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Strandjord, Lee K., Sanders, Glen A., Qiu, Tiequn
• Primary Examiner(s): Chowdhury, Tarifur
• Assistant Examiner(s): HANSEN, JONATHAN M
• Application Number:
  US12/789,972
• Publication Number:
  US 20110292396A1
• Time in Patent Office: 781 Days
• Field of Search: 356/459, 356/460, 356/461, 385/31, 385/32, 735/040.1
• US Class Current: 356/461
• CPC Class Codes: G01C 19/727 using a passive ring resonator

Abstract

A resonator fiber optic gyroscope includes a sensing resonator having a first resonance frequency for a first laser beam propagation direction and a second resonance frequency for a second laser beam propagation direction; an intensity modulator coupled to an output of the sensing resonator and configured to modulate the intensity of a signal output from the sensing resonator, wherein the intensity modulator modulates the output signal at an intensity modulation frequency; and resonance tracking electronics coupled to an output of the intensity modulator and configured to demodulate the intensity modulated signal output from the intensity modulator at a resonance tracking modulation frequency to produce a first demodulated signal; the resonance tracking electronics further configured to demodulate the first demodulated signal at the intensity modulation frequency, wherein the intensity modulation frequency is different from the resonance tracking modulation frequency.

Claims

1. A fiber optic gyroscope comprising:

a first laser source configured to produce a first laser beam having a first frequency;

a second laser source configured to produce a second laser beam having a second frequency;

a sensing resonator having a first input coupled to the first laser source and a second input coupled to the second laser source such that the first laser beam propagates through the sensing resonator in a first direction and the second laser beam propagates through the sensing resonator in a second direction;

first resonance tracking electronics (RTE) configured to generate a first control signal that indicates when the first laser beam is off resonance;

second resonance tracking electronics (RTE) configured to generate a second control signal that indicates when the second laser beam is off resonance;

a first intensity modulator coupled between a first output of the sensing resonator and an input of the first resonance tracking electronics, the first intensity modulator configured to modulate the intensity of a signal from the first output of the sensing resonator at a first intensity modulation frequency such that the first resonance tracking electronics is able to discriminate between the signal from the first output of the sensing resonator and electronic noise, wherein the first intensity modulation frequency is different from a resonance tracking modulation frequency of the first RTE; and

a second intensity modulator coupled between a second output of the sensing resonator and an input of the second resonance tracking electronics, the second intensity modulator configured to modulate the intensity of a signal from the second output of the sensing resonator at a second intensity modulation frequency such that the second resonance tracking electronics is able to discriminate between the signal from the second output of the sensing resonator and electronic noise, wherein the second intensity modulation frequency is different from a resonance tracking modulation frequency of the second RTE.

2. The fiber optic gyroscope of claim 1, wherein the fiber optic gyroscope further comprises:

a reference laser configured to produce a reference laser beam;

a first phase-lock-loop (PLL) to beat the first laser beam with the reference laser beam and to drive the first laser source such that the first laser beam is locked to the reference laser beam; and

a second phase-lock-loop (PLL) to beat the second laser beam with the reference laser beam and to drive the second laser source such that the second laser beam is locked to the reference laser beam.

3. The fiber optic gyroscope of claim 2, wherein:

the first RTE is further configured to output a first reference frequency to the first PLL to maintain the first frequency at a first resonance frequency of the sensing resonator; and

the second RTE is further configured to output a second reference frequency to the second PLL to maintain the second frequency at a second resonance frequency of the sensing resonator.

4. The fiber optic gyroscope of claim 1, further comprising:

a first preamplifier coupled between an output of the first intensity modulator and the input of the first RTE, the first preamplifier configured to convert the intensity modulated signal from the first intensity modulator to an electrical signal;

a second preamplifier coupled between an output of the second intensity modulator and the input of the second RTE, the second preamplifier configured to convert the intensity modulated signal from the second intensity modulator to an electrical signal.

5. The fiber optic gyroscope of claim 1, wherein each of the first and second RTE comprises:

a first demodulator configured to demodulate the intensity modulated signal from the respective intensity modulator at the respective resonance tracking modulation frequency; and

a second demodulator coupled to an output of the first demodulator and configured to demodulate a signal output from the first demodulator at the intensity modulation frequency of the respective intensity modulator.

6. The fiber optic gyroscope of claim 5, wherein each of the first and second demodulators is a lock-in amplifier.

7. The fiber optic gyroscope of claim 5, wherein each of the first and second RTE further comprises:

an analog-to-digital converter configured to convert the intensity modulated signal to a digital signal; and

a digital signal processor coupled to the analog-to-digital converter, wherein the digital signal processor includes the first demodulator and the second demodulator.

8. The fiber optic gyroscope of claim 7, wherein the digital signal processor of each of the first and second RTE further comprises:

a first digital signal wave generator configured to output a square wave at the respective resonance tracking modulation frequency to the first demodulator;

a second digital signal wave generator configured to output a sine wave at the respective intensity modulation frequency to the respective intensity modulator to drive the respective intensity modulator, wherein the second digital signal wave generator is further configured to output a square wave at the respective intensity modulation frequency to the second demodulator;

an accumulator configured to integrate an output of the second demodulator;

a first summer configured to sum the integrated output of the accumulator with a sine wave at the respective resonance tracking modulation frequency generated by the first digital signal wave generator; and

a second summer configured to sum an output of the first summer with a constant value.

9. The fiber optic gyroscope of claim 1 wherein the first intensity modulation frequency is not harmonically related to the resonance tracking modulation frequency of the first RTE;

and

wherein the second intensity modulation frequency is not harmonically related with the resonance tracking modulation frequency of the second RTE.

10. A system comprising:

a resonator fiber optic gyroscope configured to measure rotation rate; and

a processing unit coupled to the resonator fiber optic gyroscope and configured to perform calculations based on the rotation rate measured by the resonator fiber optic gyroscope;

wherein the resonator fiber optic gyroscope includes;

a sensing resonator having a first resonance frequency for a first laser beam propagation direction and a second resonance frequency for a second laser beam propagation direction;

an intensity modulator coupled to an output of the sensing resonator and configured to modulate the intensity of a signal output from the sensing resonator, wherein the intensity modulator modulates the output signal at an intensity modulation frequency; and

resonance tracking electronics coupled to an output of the intensity modulator and configured to demodulate the intensity modulated signal output from the intensity modulator at a resonance tracking modulation frequency to produce a first demodulated signal;

the resonance tracking electronics further configured to demodulate the first demodulated signal at the intensity modulation frequency, wherein the intensity modulation frequency is different from the resonance tracking modulation frequency.

11. The system of claim 10, wherein the resonator fiber optic gyroscope further comprises:

a first laser source coupled to a first input of the sensing resonator and configured to produce a first laser beam having a first frequency;

a second laser source coupled to a second input of the sensing resonator and configured to produce a second laser beam having a second frequency;

a reference laser configured to produce a reference laser beam;

a first phase-lock-loop (PLL) to beat the first laser beam with the reference laser beam and to drive the first laser source such that the first laser beam is locked to the reference laser beam; and

a second phase-lock-loop (PLL) to beat the second laser beam with the reference laser beam and to drive the second laser source such that the second laser beam is locked to the reference laser beam.

12. The system of claim 10, wherein the resonator fiber optic gyroscope further comprises a preamplifier coupled between an output of the intensity modulator and an input of the resonance tracking electronics, the preamplifier configured to convert the output from the intensity modulator to an electrical signal.

13. The system of claim 10, wherein the resonator fiber optic gyroscope further comprises:

an analog-to-digital converter configured to convert an output of the intensity modulated signal to a digital signal; and

a digital signal processor coupled to the analog-to-digital converter, wherein the digital signal processor includes;

a first demodulator configured to produce the first demodulated signal;

a second demodulator coupled to an output of the first demodulator and configured to demodulate the first demodulated signal at the intensity modulation frequency;

a first digital signal wave generator configured to output a square wave at the resonance tracking modulation frequency to the first demodulator; and

a second digital signal wave generator configured to output a square wave at the intensity modulation frequency to the second demodulator.

14. The system of claim 13, wherein the second digital signal wave generator is further configured to output a sine wave at the intensity modulation frequency to the intensity modulator to drive the intensity modulator.

15. The system of claim 13, wherein the digital signal processor further comprises:

an accumulator configured to integrate an output of the second demodulator;

a first summer configured to sum the integrated output of the accumulator with a sine wave at the resonance tracking modulation frequency generated by the first digital signal wave generator; and

a second summer configured to sum an output of the first summer with a constant value.

16. The system of claim 10, wherein the intensity modulation frequency is not harmonically related with the resonance tracking modulation frequency.

17. A method of enhancing signal-to-noise ratio for measuring rotation rate in a resonator fiber optic gyroscope, the method comprising:

modulating intensity of a signal output from a sensing resonator, wherein the intensity is modulated at an intensity modulation frequency that is different from a resonance tracking modulation frequency;

demodulating the intensity modulated signal at the intensity modulation frequency and at the resonance tracking modulation frequency to produce a double demodulated signal; and

generating a signal related to rotation rate based on the double demodulated signal.

18. The method of claim 17, wherein demodulating the intensity modulated signal comprises one of:

demodulating the intensity modulated signal at the resonance tracking modulation frequency to produce a first demodulated signal and demodulating the first demodulated signal at the intensity modulation frequency to produce the double demodulated signal;

or

demodulating the intensity modulated signal at the intensity modulation frequency to produce a first demodulated signal and demodulating the first demodulated signal at the resonance tracking modulation frequency to produce the double demodulated signal.

19. The method of claim 17, wherein modulating intensity of the signal output from the sensing resonator comprises:

modulating intensity of the signal output from the sensing resonator at an intensity modulation frequency that is not harmonically related to a resonance tracking modulation frequency.

20. The method of claim 17, wherein generating a signal related to rotation rate comprises:

integrating the double demodulated signal;

summing the integrated signal with a sine wave at the resonance tracking modulation frequency to produce a first summed signal; and

summing the first summed signal with a constant value representing a nominal beat frequency to produce the signal related to rotation rate.