Methods and apparatus of tracking/locking resonator free spectral range and its application in resonator fiber optic gyroscope

• US 9,001,336 B1
• Filed: 10/07/2013
• Issued: 04/07/2015
• Est. Priority Date: 10/07/2013
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Qiu, Tiequn, Strandjord, Lee K., Sanders, Glen A., Wu, Jianfeng
• Primary Examiner(s): Chowdhury, Tarifur
• Assistant Examiner(s): Nixon, Omar
• Application Number:
  US14/047,855
• Publication Number:
  US 20150098088A1
• Time in Patent Office: 547 Days
• Field of Search: 356/461
• US Class Current: 356/461
• CPC Class Codes: G01C 19/661 details
• CPC Class Codes: G01C 19/727 using a passive ring resonator

Abstract

A resonator fiber optic gyroscope is provided. The resonator fiber optic gyroscope includes a gyroscope resonator, a laser; a clockwise modulator; a clockwise circulator; a clockwise reflection detector; a first-lock-in-amplifier, a clockwise-resonance-tracking servo to receive output from the first-lock-in-amplifier and to provide feedback to the laser to lock the laser to the gyroscope resonator; a clockwise transmission detector to detect an optical beam output from the counter-clockwise input port; a second servo; a second-lock-in-amplifier; and a third-lock-in-amplifier. The first and second lock-in-amplifiers demodulate at the first harmonic of the modulation frequency. The second-lock-in-amplifier demodulates at the second harmonic of the modulation frequency. Either the modulation frequency of the clockwise optical beam is locked to (n+0.5) times the FSR through the second servo, where n is zero or a positive integer, or the FSR is locked to 1/(n+0.5) times the modulation frequency of the clockwise optical beam through the second servo.

Claims

1. A resonator fiber optic gyroscope system, comprising:

a gyroscope resonator having a clockwise input port and a counter-clockwise input port and a free spectral range (FSR) corresponding to the resonator round trip length;

a laser configured to couple a clockwise optical beam into to the clockwise input port;

a clockwise modulator to impose a modulation frequency equivalent to (n+0.5) times the FSR on the clockwise optical beam before the clockwise optical beam is coupled into the clockwise input port, where n is zero or a positive integer;

a clockwise circulator;

a clockwise reflection detector to detect the clockwise optical beam output from a clockwise reflection port;

a first-lock-in-amplifier to receive a signal from the clockwise reflection detector, wherein the first-lock-in-amplifier demodulates at the first harmonic of the modulation frequency of the clockwise optical beam;

a clockwise-resonance-tracking servo to receive output from the first-lock-in-amplifier and to provide feedback to the laser to lock the laser to the gyroscope resonator;

a clockwise transmission detector to detect an optical beam output from the counter-clockwise input port;

a second servo;

a second-lock-in-amplifier to receive a signal from the clockwise transmission detector, wherein the second-lock-in-amplifier demodulates at the second harmonic of the modulation frequency of the clockwise optical beam and provides feedback to the second servo; and

a third-lock-in-amplifier to receive a signal from the clockwise transmission detector, wherein the third-lock-in-amplifier demodulates at the first harmonic of the modulation frequency of the clockwise optical beam and provides feedback to the clockwise-resonance-tracking servo to correct errors in a clockwise resonance tracking loop,

wherein one of;

the modulation frequency of the clockwise optical beam is locked to (n+0.5) times the FSR through the second servo, where n is zero or a positive integer;

or the FSR is locked to 1/(n+0.5) times the modulation frequency of the clockwise optical beam through the second servo.

2. The resonator fiber optic gyroscope system of claim 1, wherein the laser is a first laser, further comprising:

a second laser configured to couple a counter-clockwise optical beam into to the counter-clockwise input port;

a counter-clockwise modulator to impose a modulation frequency equivalent to (p+0.5) times the FSR on the counter-clockwise optical beam before the counter-clockwise optical beam is coupled into the counter-clockwise input port, where p is zero or a positive integer and where p does not equal n;

a counter-clockwise circulator;

a counter-clockwise reflection detector to detect the counter-clockwise optical beam output from a counter-clockwise reflection port;

a fourth-lock-in-amplifier to receive a signal from the counter-clockwise reflection detector, wherein the fourth-lock-in-amplifier demodulates at the first harmonic of the modulation frequency of the counter-clockwise optical beam;

a counter-clockwise-resonance-tracking servo to receive output from the fourth-lock-in-amplifier and to provide feedback to the second laser to lock the second laser to the gyroscope resonator;

a counter-clockwise transmission detector to detect an optical beam output from the clockwise input port; and

the fifth-lock-in-amplifier to receive a signal from the counter-clockwise transmission detector, wherein the fifth-lock-in-amplifier demodulates at the first harmonic of the modulation frequency of the counter-clockwise optical beam and provides feedback to the counter-clockwise-resonance-tracking servo to correct errors in a counter-clockwise resonance tracking loop.

3. The resonator fiber optic gyroscope system of claim 2, wherein the second servo is a free-spectral-range (FSR) servo, the resonator fiber optic gyroscope system further comprising:

a piezo-electric device to input feedback from the FSR servo, wherein a length of a gyroscope resonator coil is changed by the piezo-electric device to adjust the FSR of the gyroscope resonator in order to lock the FSR in relation to the modulation frequency of the clockwise optical beam.

4. The resonator fiber optic gyroscope system of claim 3, wherein FSR servo further provides a temperature control signal to the gyroscope resonator based on the feedback from the second-lock-in-amplifier.

5. The resonator fiber optic gyroscope system of claim 2, wherein the second servo is a modulation-frequency servo, the resonator fiber optic gyroscope system further comprising:

a clockwise tunable modulation generator to drive the clockwise modulator; and

a counter-clockwise tunable modulation generator to drive the counter-clockwise modulator,

wherein the clockwise tunable modulation generator receives feedback from the modulation-frequency servo to adjust the modulation frequency of the clockwise optical beam as the FSR changes in order to lock the modulation frequency of the clockwise optical beam to the (n+0.5)FSR, and

wherein the counter-clockwise tunable modulation generator receives feedback from the modulation-frequency servo to adjust the modulation frequency of the counter-clockwise optical beam as the FSR changes in order to lock the modulation frequency of the counter-clockwise optical beam to the (p+0.5)FSR.

6. The resonator fiber optic gyroscope system of claim 1, wherein the second servo is a FSR servo, the resonator fiber optic gyroscope system further comprising:

a piezo-electric device to input feedback from the FSR servo, wherein a length of a gyroscope resonator coil is changed by the piezo-electric device to adjust the FSR of the gyroscope resonator in order to lock the FSR in relation to the modulation frequency of the clockwise optical beam.

7. The resonator fiber optic gyroscope system of claim 1, wherein the second servo is a modulation-frequency servo, the resonator fiber optic gyroscope system further comprising:

a clockwise tunable modulation generator configured to drive the clockwise phase modulator, wherein the clockwise tunable modulation generator receives feedback from the modulation-frequency servo to adjust the modulation frequency of the clockwise optical beam as the FSR changes in order to lock the modulation frequency of the clockwise optical beam to the (n+0.5)FSR.

8. The resonator fiber optic gyroscope system of claim 1, further comprising:

a photodetector to receive a portion of the clockwise optical beam combined with a portion of the counter-clockwise optical beam to generate a beat signal from the combined optical beams; and

a processing unit to calculate a rotation rate based on at least the beat signal.

9. A method of locking a free spectral range (FSR) of a gyroscope resonator in a resonator fiber optic gyroscope system and a laser modulation frequency of an optical beam coupled to an input port of the gyroscope resonator to each other, the method comprising:

modulating a clockwise optical beam emitted from a laser with a laser modulation frequency of (n+0.5) times the FSR, where n is zero or a positive integer;

coupling the modulated clockwise optical beam into a clockwise input port of the gyroscope resonator;

receiving a signal from a clockwise reflection detector;

demodulating a first harmonic of the signal received from the clockwise reflection detector at a first-lock-in-amplifier;

receiving a demodulated first-harmonic signal from the first-lock-in-amplifier at a clockwise-resonance-tracking servo;

providing feedback to the laser from the clockwise-resonance-tracking servo in order to lock the laser to the gyroscope resonator;

receiving a signal from a clockwise transmission detector;

demodulating a second harmonic of the signal received from the clockwise transmission detector at a second-lock-in-amplifier;

providing feedback from the second-lock-in-amplifier to a second servo;

demodulating a first harmonic of the signal received from the clockwise transmission detector at a third-lock-in-amplifier; and

providing feedback from the third-lock-in-amplifier to the clockwise-resonance-tracking servo to correct errors in a clockwise resonance tracking loop.

10. The method of claim 9, wherein the laser is a first laser, the method further comprising:

modulating a counter-clockwise optical beam emitted from a second laser with a laser modulation frequency of (p+0.5) times the FSR, where p is zero or a positive integer and p does not equal n;

coupling the modulated counter-clockwise optical beam into a counter-clockwise input port of the gyroscope resonator;

receiving a signal from a counter-clockwise reflection detector at a fourth-lock-in-amplifier;

demodulating a first harmonic of the signal received from the counter-clockwise reflection detector at the fourth-lock-in-amplifier;

receiving a demodulated first-harmonic signal from the fourth-lock-in-amplifier at a counter-clockwise-resonance-tracking servo; and

providing feedback to the second laser from the counter-clockwise-resonance-tracking servo to lock the second laser to the gyroscope resonator.

11. The method of claim 10, further comprising:

receiving a signal from counter-clockwise transmission detector at a fifth-lock-in-amplifier;

demodulating a first harmonic of the signal received from the counter-clockwise transmission detector at the fifth-lock-in-amplifier; and

providing feedback from the fifth-lock-in-amplifier to the counter-clockwise-resonance-tracking servo to correct errors in the counter-clockwise resonance tracking loop.

12. The method of claim 10, wherein the second servo is a FSR servo, the method further comprising:

providing feedback from the FSR servo to a piezo-electric device based on the feedback from the second-lock-in-amplifier;

adjusting a length of a gyroscope resonator coil by driving the piezo-electric device based on the feedback received at the FSR device; and

locking the FSR to 1/(n+0.5) times the modulation frequency of the clockwise optical beam through the adjustment to the length of the gyroscope resonator coil.

13. The method of claim 12, further comprising:

providing a temperature control signal to the gyroscope resonator from the FSR servo based on the feedback from the second-lock-in-amplifier.

14. The method of claim 10, wherein the second servo is a modulation-frequency servo, the method further comprising:

providing feedback from the modulation-frequency servo to a clockwise tunable modulation generator based on the feedback from the second-lock-in-amplifier;

adjusting the modulation frequency of the clockwise optical beam as the FSR changes to lock the modulation frequency of the clockwise optical beam to the (n+0.5)FSR;

providing feedback from the modulation-frequency servo to a counter-clockwise tunable modulation generator based on the feedback from the second-lock-in-amplifier; and

adjusting the modulation frequency of the counter-clockwise optical beam as the FSR changes to lock the modulation frequency of the counter-clockwise optical beam to the (p+0.5)FSR.

15. The method of claim 9, wherein the second servo is a FSR servo, the method further comprising:

providing feedback from the FSR servo to a piezo-electric device based on the feedback from the second-lock-in-amplifier;

adjusting a length of a gyroscope resonator coil by implementing the piezo-electric device based on the feedback received at the piezo-electric device; and

locking the FSR to the modulation frequency of the clockwise optical through the adjustment to the length of the gyroscope resonator coil.

16. The method of claim 15, further comprising:

providing a temperature control signal to the gyroscope resonator from the FSR servo based on the feedback from the second-lock-in-amplifier.

17. The method of claim 9, wherein the second servo is a modulation-frequency servo, the resonator fiber optic gyroscope further comprises:

providing feedback from the modulation-frequency servo to a clockwise tunable modulation generator based on the feedback from the second-lock-in-amplifier;

adjusting the modulation frequency of the clockwise optical beam as the FSR changes to lock the modulation frequency of the clockwise optical beam to the (n+0.5)FSR;

providing feedback from the modulation-frequency servo to a counter-clockwise tunable modulation generator based on the feedback from the second-lock-in-amplifier; and

adjusting the modulation frequency of the counter-clockwise optical beam as the FSR changes to lock the modulation frequency of the counter-clockwise optical beam to (p+0.5)FSR.

18. A resonator fiber optic gyroscope system, comprising:

a gyroscope resonator having a clockwise input port and a counter-clockwise input port and a free spectral range (FSR) corresponding to the resonator round trip length;

a first laser configured to couple a clockwise optical beam into to the clockwise input port;

a clockwise modulator to impose a modulation frequency equivalent to (n+0.5) times the FSR on the clockwise optical beam before the clockwise optical beam is coupled into the clockwise input port, where n is a positive integer;

a clockwise circulator;

a clockwise reflection detector to detect the clockwise optical beam output from a clockwise reflection port;

a first-lock-in-amplifier to receive a signal from the clockwise reflection detector, wherein the first-lock-in-amplifier demodulates at the first harmonic of the modulation frequency of the clockwise optical beam;

a clockwise-resonance-tracking servo to receive output from the first-lock-in-amplifier and to provide feedback to the first laser to lock the first laser to the gyroscope resonator;

a clockwise transmission detector to detect an optical beam output from the counter-clockwise input port;

a second servo;

a second-lock-in-amplifier to receive a signal from the clockwise transmission detector, wherein the second-lock-in-amplifier demodulates at the second harmonic of the modulation frequency of the clockwise optical beam and provides feedback to the second servo;

a third-lock-in-amplifier to receive a signal from the clockwise transmission detector, wherein the third-lock-in-amplifier demodulates at the first harmonic of the modulation frequency of the clockwise optical beam and provides feedback to the clockwise-resonance-tracking servo to correct errors in a clockwise resonance tracking loop,

a second laser configured to couple a counter-clockwise optical beam into to the counter-clockwise input port;

a counter-clockwise modulator to impose a modulation frequency equivalent to (p+0.5) times the FSR on the counter-clockwise optical beam before the counter-clockwise optical beam is coupled into the counter-clockwise input port, where p is zero or a positive integer and where p does not equal n;

a counter-clockwise circulator;

a counter-clockwise reflection detector to detect the counter-clockwise optical beam output from a counter-clockwise reflection port;

a fourth-lock-in-amplifier to receive a signal from the counter-clockwise reflection detector, wherein the fourth-lock-in-amplifier demodulates at the first harmonic of the modulation frequency of the counter-clockwise optical beam;

a counter-clockwise-resonance-tracking servo to receive output from the fourth-lock-in-amplifier and to provide feedback to the second laser to lock the second laser to the gyroscope resonator;

a counter-clockwise transmission detector to detect an optical beam output from the clockwise input port; and

the fifth-lock-in-amplifier to receive a signal from the counter-clockwise transmission detector, wherein the fifth-lock-in-amplifier demodulates at the first harmonic of the modulation frequency of the counter-clockwise optical beam and provides feedback to the counter-clockwise-resonance-tracking servo to correct errors in a counter-clockwise resonance tracking loop,

wherein one of;

the modulation frequency of the clockwise optical beam is locked to the (n+0.5)FSR through the second servo;

or the FSR is locked to 1/(n+0.5) times the modulation frequency of the clockwise optical beam through the second servo.

19. The resonator fiber optic gyroscope system of claim 18, wherein the second servo is a FSR servo, the resonator fiber optic gyroscope system further comprising:

a piezo-electric device to input feedback from the FSR servo, wherein a length of a gyroscope resonator coil is changed by the piezo-electric device to adjust the FSR of the gyroscope resonator based on the feedback from the FSR servo to lock the FSR in relation to the modulation frequency of the clockwise optical beam.

20. The resonator fiber optic gyroscope system of claim 18, wherein the second servo is a modulation-frequency servo, the resonator fiber optic gyroscope system further comprising:

a clockwise tunable modulation generator to drive the clockwise phase modulator; and

a counter-clockwise modulation to drive the counter-clockwise phase modulator,

wherein the clockwise tunable modulation generator receives feedback from the modulation-frequency servo to adjust the modulation frequency of the clockwise optical beam as the FSR changes, wherein the modulation frequency of the clockwise optical beam is locked to the (n+0.5)FSR, and

wherein the counter-clockwise tunable modulation generator receives feedback from the modulation-frequency servo to adjust the modulation frequency of the counter-clockwise optical beam as the FSR changes, wherein the modulation frequency of the counter-clockwise optical beam is locked to (p+0.5)FSR.