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Resonant type fiber-optic gyro coherent demodulation system and method based on interference of externally added light beams

A technology of beam and source resonance, applied in the direction of Sagnac effect gyroscope, etc., can solve the problems that the frequency noise of the laser cannot be completely suppressed, the large frequency noise of the semiconductor laser, etc., so as to reduce the frequency noise of the laser, clear the spectrum of the signal, increase the The effect of a large signal-to-noise ratio

Active Publication Date: 2018-07-27
ZHEJIANG UNIV
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Problems solved by technology

[0006] From the perspective of system miniaturization, a semiconductor laser with a smaller volume is more suitable as a system light source for a resonant fiber optic gyroscope, but the semiconductor laser itself has greater frequency noise than a fiber laser, and the PDH laser frequency locking technology is limited Due to the noise suppression bandwidth, it only has a good suppression effect on frequency noise at low frequencies, and has no suppression effect on white noise at high frequencies.
Therefore, the existing laser frequency noise suppression scheme cannot completely suppress the laser frequency noise in the miniaturized resonator fiber optic gyroscope

Method used

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  • Resonant type fiber-optic gyro coherent demodulation system and method based on interference of externally added light beams

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Embodiment Construction

[0022] Such as figure 1 As shown, a resonant fiber optic gyroscope coherent demodulation system based on external beam interference includes a laser 1, a first polarization-maintaining coupler 2, a Y-branch phase modulator 3, a phase modulator 4, a fiber resonator 5, and a second protection Polarization coupler 6, third polarization maintaining coupler 7, first photodetector 8, first bandpass filter 9, second photodetector 10, local carrier generation module 10, first local carrier phase shift module 11, 90° phase shift module 12, first multiplier 13, second multiplier 14, first low-pass filter 15, second low-pass filter 16, third multiplier 17, third low-pass filter 18, first A digital lock-in amplifier 19, PI servo loop 20, fourth polarization-maintaining coupler 21, second photodetector 22, second bandpass filter 23, second local carrier phase shift module 24, second 90° phase shift Module 25, fourth multiplier 26, fifth multiplier 27, fourth low pass filter 28, fifth low p...

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Abstract

The invention discloses a resonant type fiber-optic gyro coherent demodulation system and method based on interference of externally added light beams. The system includes a laser, a first polarization-maintaining coupler, a Y-branch phase modulator, a phase modulator, an optical fiber resonant cavity, a second polarization-maintaining coupler, a third polarization-maintaining coupler, a first photoelectric detector, a first band-pass filter, a local carrier generation module, a first local carrier phase shift module, a first 90-degree phase shift module, a first multiplier, a second multiplier, a first low-pass filter, a second low-pass filter, a third multiplier, a third low-pass filter, a first digital phase-lock amplifier, a PI servo loop, a fourth polarization-maintaining coupler, a second photoelectric detector, a second band-pass filter, a second local carrier phase shift module, a second 90-degree phase shift module, a fourth multiplier, a fifth multiplier, a fourth low-pass filter, a fifth low-pass filter, a sixth multiplier, a sixth low-pass filter, and a second digital phase-lock amplifier. By local recovery of a carrier with high signal-to-noise ratio, the signal-to-noise ratio of a demodulated signal is improved, the influence of laser frequency noise is reduced, and the resonant type fiber-optic gyro coherent demodulation system and method have important scientific significance and application value.

Description

Technical field [0001] The invention relates to a resonant fiber optic gyroscope demodulation system and method for locking the resonant cavity of an optical passive resonator through external coherent light interference, so as to suppress the laser frequency noise in the resonant fiber optic gyroscope. Background technique [0002] The resonant fiber optic gyroscope is an inertial angular velocity sensor based on the Sagnac effect. It uses the frequency difference between the clockwise and counterclockwise resonant frequencies of the resonant cavity caused by the Sagnac phase shift caused by rotation to measure the rotational angular velocity. Compared with interferometric fiber optic gyroscopes, resonant fiber optic gyroscopes use lasers to transmit multiple times in a resonant cavity to amplify the Sagnac effect and achieve the same ultimate sensitivity as the interferometric fiber optic gyroscopes by using shorter fibers. It has the characteristics of high precision, high tem...

Claims

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Application Information

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IPC IPC(8): G01C19/72
CPCG01C19/72
Inventor 金仲和李汉钊马慧莲
Owner ZHEJIANG UNIV
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