Laser-driven optical gyroscope with push-pull modulation
US-2015022818-A1 · Jan 22, 2015 · US
US10228250B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10228250-B2 |
| Application number | US-201715707343-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 18, 2017 |
| Priority date | Sep 20, 2016 |
| Publication date | Mar 12, 2019 |
| Grant date | Mar 12, 2019 |
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An optical system is provided having a laser configured to generate light having a first laser spectrum with a first linewidth, a waveform generator configured to produce a noise waveform, and an electro-optic phase modulator in optical communication with the laser and in electrical communication with the waveform generator. The electro-optic phase modulator is configured to receive the light having the first laser spectrum, to receive the noise waveform, and to respond to the noise waveform by modulating the light to produce light having a second laser spectrum with a second linewidth broader than the first linewidth.
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What is claimed is: 1. An optical system comprising: a laser configured to generate light having a first laser spectrum with a first linewidth; a waveform generator configured to produce a noise waveform, the waveform generator comprising at least one noise source and at least one amplifier configured to amplify a source noise waveform from the at least one noise source to produce the noise waveform, the at least one amplifier having a saturation voltage level V sat ; and an electro-optic phase modulator in optical communication with the laser and in electrical communication with the waveform generator, the electro-optic phase modulator configured to receive the light having the first laser spectrum, to receive the noise waveform, and to respond to the noise waveform by modulating the light to produce light having a second laser spectrum with a second linewidth broader than the first linewidth, the electro-optic phase modulator having a voltage V π at which the electro-optic phase modulator produces a π-phase shift, wherein the saturation voltage level V sat and the voltage V π have a ratio V sat /V π selected to minimize a power fraction f c of the first laser spectrum in the second laser spectrum. 2. The optical system of claim 1 , wherein the laser comprises a single-transverse mode laser. 3. The optical system of claim 1 , wherein the noise waveform is a Gaussian white-noise waveform. 4. The optical system of claim 3 , wherein the Gaussian white-noise waveform has a cutoff bandwidth and a substantially constant power spectral density for frequencies between zero and the cutoff bandwidth. 5. The optical system of claim 1 , wherein the at least one amplifier comprises one or more RF amplifiers. 6. The optical system of claim 1 , wherein V sat has a peak-to-peak value such that V sat /V π is within ±10% of an odd integer. 7. The optical system of claim 1 , further comprising a sensor in optical communication with the electro-optic phase modulator and configured to receive the light having the second laser spectrum. 8. The optical system of claim 7 , wherein the sensor comprises a fiber-optic gyroscope. 9. The optical system of claim 8 , wherein the fiber-optic gyroscope comprises a multifunction integrated-optic chip (MIOC) and a sensing coil in optical communication with the MIOC, the MIOC in optical communication with the electro-optic phase modulator and configured to receive the light from the electro-optic phase modulator. 10. The optical system of claim 9 , wherein the MIOC comprises a polarizer, a Y-junction, and push-pull phase modulators driven by a square-wave modulation signal at the loop proper frequency. 11. The optical system of claim 9 , wherein the sensing coil comprises a quadrupolar-wound polarization-maintaining fiber having a coil length greater than 1 kilometer. 12. The optical system of claim 9 , wherein the MIOC and the sensing coil are contained within a thermally isolated enclosure. 13. The optical system of claim 8 , wherein the fiber-optic gyroscope has a noise level less than 0.001 degree/(hour) 1/2 and a drift level less than 0.01 degree/hour. 14. The optical system of claim 8 , wherein the fiber-optic gyroscope has an angular random walk below 0.001 degree/(hour) 1/2 and a bias error drift below 0.01 degree/hour. 15. The optical system of claim 1 , wherein the power fraction f c of the first laser spectrum in the second laser spectrum is below 1%. 16. The optical system of claim 1 , wherein the power fraction f c of the first laser spectrum in the second laser spectrum is less than or equal to −13 dB. 17. A method of producing laser-based broadband light for use in an optical device, the method comprising: using a laser to generate light having a first laser spectrum with a first linewidth; producing a noise waveform using a waveform generator comprising at least one noise source and at least one amplifier configured to amplify a source noise waveform from the at least one noise source to produce the noise waveform, the at least one amplifier having a saturation voltage level V sat ; and in response to the noise waveform, using an electro-optic phase modulator in optical communication with the laser and in electrical communication with the waveform generator to modulate the light to have a second laser spectrum with a second linewidth broader than the first linewidth, the electro-optic phase modulator having a voltage V π at which the electro-optic phase modulator produces a π-phase shift, wherein the saturation voltage level V sat and the voltage V π have a ratio V sat /V π selected to minimize a power fraction f c of the first laser spectrum in the second laser spectrum. 18. The method of claim 17 , wherein the noise waveform is a Gaussian white-noise waveform. 19. The method of claim 18 , wherein the Gaussian white-noise waveform has a cutoff bandwidth and a substantially constant power spectral density for frequencies between zero and the cutoff bandwidth. 20. The method of claim 17 , further comprising inputting the light having the second laser spectrum into a sensor. 21. The method of claim 20 , wherein the sensor comprises a fiber-optic gyroscope. 22. The method of claim 21 , wherein the fiber-optic gyroscope has a noise level less than 0.001 degree/(hour) 1/2 and a drift level less than 0.01 degree/hour. 23. The method of claim 21 , wherein the fiber-optic gyroscope has an angular random walk below 0.001 degree/(hour) 1/2 and a bias error drift below 0.01 degree/hour. 24. The method of claim 17 , wherein the power fraction f c of the first laser spectrum in the second laser spectrum is below 1%. 25. The method of claim 17 , wherein the power fraction f c of the first laser spectrum in the second laser spectrum is less than or equal to −13 dB.
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Operation of devices; Circuit arrangements, not otherwise provided for in this subclass · CPC title
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Modulating the output, i.e. the laser beam is modulated outside the laser cavity · CPC title
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