Photonics gyroscope with broadband light source

Patent metadata

Field	Value
Publication number	US-12345530-B2
Application number	US-202318193448-A
Country	US
Kind code	B2
Filing date	Mar 30, 2023
Priority date	Mar 30, 2023
Publication date	Jul 1, 2025
Grant date	Jul 1, 2025

Abstract

A photonics gyroscope comprises a light source on a photonics chip that emits a broadband beam; a waveguide resonator; a reflective component; first and second detectors, the second detector coupled to the source; a RIN servo loop coupled between the second detector and the source; and a rate calculation unit. The beam is directed into the resonator such that it propagates in a CCW direction. A portion of the CCW beam is coupled out of the resonator toward the reflective component and reflected back as a reflected beam that is coupled into the resonator such that the reflected beam propagates in a CW direction. The CW beam is coupled out of the resonator to the first detector, which detects a resonance frequency shift between the CW and CCW beams. The RIN servo loop stabilizes an intensity of the beam such that bias error and noise is reduced.

First claim

What is claimed is:

1. A photonics gyroscope, comprising:
a light source on a photonics chip, the light source configured to emit a light beam with a broadband spectrum;
a waveguide resonator on the photonics chip, the waveguide resonator in optical communication with the light source through an optical path provided by a first waveguide arrangement comprising a first waveguide optically coupled to an output of the light source, and a second waveguide optically coupled to the waveguide resonator;
a first phase modulator on the photonics chip and in optical communication with the waveguide resonator through the first waveguide arrangement;
a reflective component on the photonics chip and in optical communication with the waveguide resonator;
a first optical detector on the photonics chip and in optical communication with the waveguide resonator, wherein the second waveguide is optically coupled between the first phase modulator and an input of the first optical detector;
a second optical detector on the photonics chip and operatively coupled to the light source; and
a relative intensity noise (RIN) servo loop coupled between an output of the second optical detector and an input of the light source.

2. The photonics gyroscope of claim 1 , wherein the light source comprises an amplified spontaneous emission device, a superluminescent diode, or two or more superluminescent diodes having different center wavelengths.

3. The photonics gyroscope of claim 1 , wherein the waveguide resonator comprises a waveguide ring resonator.

4. The photonics gyroscope of claim 1 , wherein the reflective component comprises a Bragg grating, or an edge high reflective coating on a waveguide edge.

5. The photonics gyroscope of claim 1 , wherein:
a portion of the first waveguide is optically coupled to a portion of the second waveguide at a first coupler region; and
the second waveguide is optically coupled to the waveguide resonator at a second coupler region on a first side of the waveguide resonator.

6. The photonics gyroscope of claim 5 , wherein the reflective component is in optical communication with the waveguide resonator through a second waveguide arrangement.

7. The photonics gyroscope of claim 6 , further comprising:
a second phase modulator on the photonics chip and in optical communication with the waveguide resonator through the second waveguide arrangement; and
a third phase modulator on the photonics chip and in optical communication with the waveguide resonator through the second waveguide arrangement.

8. The photonics gyroscope of claim 7 , further comprising:
a function generator configured to send a control signal to the third phase modulator to adjust a phase modulation frequency; and
a mixer configured to receive a signal from the function generator and an output signal from the first optical detector;
wherein the mixer combines the signals from the function generator and the first optical detector to produce a combined signal.

9. The photonics gyroscope of claim 7 , wherein the second waveguide arrangement comprises:
a third waveguide optically coupled between the second phase modulator and the third phase modulator; and
a fourth waveguide optically coupled between the reflective component and the third phase modulator.

10. The photonics gyroscope of claim 7 , wherein a low frequency modulation is applied to the phase modulators to scramble the phase of reflected beams at the phase modulators, thereby allowing the phase modulators to reduce the bias error due to parasitic interference.

11. The photonics gyroscope of claim 9 , wherein the third waveguide is optically coupled to the waveguide resonator at a third coupler region on a second side of the waveguide resonator.

12. The photonics gyroscope of claim 9 , wherein the third waveguide is optically coupled to a portion of a fifth waveguide at a fourth coupler region, the fifth waveguide optically coupled between the second optical detector and a third optical detector.

13. The photonics gyroscope of claim 12 , wherein the third optical detector is configured to monitor power of the reflected beam.

14. The photonics gyroscope of claim 5 , wherein the first waveguide is optically coupled between the light source and the second optical detector.

15. The photonics gyroscope of claim 1 , wherein:
the light beam from the light source is directed into the waveguide resonator such that the light beam propagates in a counterclockwise (CCW) direction as a CCW beam in the waveguide resonator;
a beam portion of the CCW beam is coupled out of the waveguide resonator toward the reflective component and reflected back by the reflective component as a reflected beam that is optically coupled into the waveguide resonator such that the reflected beam propagates in a clockwise (CW) direction as a CW beam in the waveguide resonator; and
the CW beam is coupled out of the waveguide resonator and directed to the first optical detector, which is operative to detect a resonance frequency shift between the CW and CCW beams caused by rotation of the photonics gyroscope.

16. The photonics gyroscope of claim 15 , wherein the RIN servo loop is configured to stabilize an intensity of the light beam emitted from the light source such that a bias error and noise in the photonics gyroscope is reduced.

17. A photonics gyroscope, comprising:
a light source on a photonics chip, the light source configured to emit a light beam with a broadband spectrum;
a waveguide ring resonator on the photonics chip, the waveguide ring resonator in optical communication with the light source through an optical path provided by a first waveguide arrangement;
a first phase modulator on the photonics chip and in optical communication with the waveguide ring resonator through the first waveguide arrangement;
a reflective component on the photonics chip and in optical communication with the waveguide ring resonator through a second waveguide arrangement;
a second phase modulator on the photonics chip and in optical communication with the waveguide ring resonator through the second waveguide arrangement;
a third phase modulator on the photonics chip and in optical communication with the waveguide ring resonator through the second waveguide arrangement;
a first optical detector on the photonics chip and in optical communication with the waveguide ring resonator and the first phase modulator through the first waveguide arrangement;
a second optical detector on the photonics chip and operatively coupled to the light source;
a relative intensity noise (RIN) servo loop coupled between an output of the second optical detector and an input of the light source;
a function generator configured to send a control signal to the third phase modulator to adjust a phase modulation frequency;
a mixer configured to receive a signal from the function generator and an output signal from the first optical detector, wherein the mixer is configured to combine the received signals to produce a combined signal; and
a rate calculation unit configured to receive the combined signal from the mixer, the rate calculation unit operative to calculate a rotation rate signal for the photonics gyroscope;
wherein the light beam from the light source is directed into the waveguide ring resonator by the first waveguide arrangement such that the light beam propagates in a counterclockwise (CCW) direction as a CCW beam in the waveguide ring resonator;
wherein a beam portion of the CCW beam is coupled out of the waveguide resonator into the second waveguide arrangement and toward the

Assignees

• Honeywell Int Inc

Inventors

• Wu Jianfeng
• Qiu Tiequn
• Puckett Matthew Wade
• Tin Steven
• Sanders Glen A

Classifications

• H01S3/0071

  Beam steering, e.g. whereby a mirror outside the cavity is present to change the beam direction · CPC title

• G01C19/722

  of the mechanical construction · CPC title

• G01C19/727 Primary

  using a passive ring resonator · CPC title