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Alternating-current frequency stabilization system and method for four-frequency laser gyroscope

A four-frequency laser gyroscope and frequency stabilization technology, applied in the field of laser gyroscopes, can solve problems such as the non-ideal symmetry of the gain curve, difficulties in mirror coating, and high requirements for transparent balance, so as to reduce the difficulty of coating, simplify frequency stabilization control, and avoid stabilization. The effect of frequency deviation

Active Publication Date: 2014-11-12
FLIGHT AUTOMATIC CONTROL RES INST
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Problems solved by technology

There are four problems in light intensity difference and frequency stabilization. One is that the transmission balance of the plane mirror 2 is relatively high (the transmission of S light is as close as possible to the transmission of P light). The transmission is very different, which brings great difficulties to the coating of the mirror
The fourth is that the actual gain curve is not ideally symmetrical, so this method of frequency stabilization will cause deviations

Method used

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  • Alternating-current frequency stabilization system and method for four-frequency laser gyroscope
  • Alternating-current frequency stabilization system and method for four-frequency laser gyroscope
  • Alternating-current frequency stabilization system and method for four-frequency laser gyroscope

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Embodiment Construction

[0037] The present invention will be described in further detail below.

[0038] Please also see image 3 and Figure 4 ,in, image 3 It is a schematic diagram of the four-frequency laser gyro AC frequency stabilization method of the present invention, Figure 4 It is a functional block diagram of the four-frequency laser gyro AC frequency stabilization system of the present invention. The four-frequency laser gyro frequency stabilization system of the present invention includes a four-frequency laser gyro and an AC frequency stabilization circuit. Among them, the four-frequency laser gyro includes two plane mirrors (partial transmission, both partial transmission and partial reflection, the ratio of the two is not strictly limited, and can be adjusted accordingly according to the actual situation) 1, 2 and two groups for controlling the length of the cavity Spherical mirrors 3 and 4 with frequency-stabilized piezoelectric ceramics. The AC frequency stabilization circuit ...

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Abstract

The invention belongs to a laser gyroscope technology, and relates to a frequency stabilization system and method for a four-frequency laser gyroscope. The frequency stabilization system for the four-frequency laser gyroscope comprises a four-frequency laser gyroscope and an alternating-current frequency stabilization circuit, wherein the four-frequency laser gyroscope comprises two planar mirrors and two groups of spherical mirror for controlling a cavity length; the alternating-current frequency stabilization circuit comprises a photoelectric converter, a band-pass filter, a phase-sensitive detector, a rectifier, a PID (Proportion Integration Differentiation) controller, a summator and a voltage amplifier; and the voltage amplifier is connected with frequency stabilization piezoelectric ceramics of the two spherical mirrors. In the invention, the cavity length of the four-frequency laser gyroscope is modulated by applying an alternating-current voltage signal to the frequency stabilization piezoelectric ceramics, a frequency stabilization error signal is obtained by performing band-pass filtering and phase-sensitive demodulation and rectification, and the error signal is stabilized at a zero value through closed loop control, so that frequency stabilization of the four-frequency laser gyroscope is realized. Due to the adoption of the system and the method, frequency stabilization control of the four-frequency laser gyroscope is simplified greatly, and the frequency stabilization accuracy is increased greatly.

Description

technical field [0001] The invention belongs to laser gyro technology, and relates to a four-frequency laser gyro frequency stabilization system and a frequency stabilization method. Background technique [0002] Laser gyroscope is an optical gyroscope based on Sagnac effect. When the carrier rotates at a speed of Ω relative to the inertial space, the laser gyroscope will generate a beat frequency output proportional to the speed, as shown in formula (1): [0003] Δν = 4 A Lλ Ω = KΩ - - - ( 1 ) [0004] Where: Δν is the beat frequency [0005] A is the area enclosed by the ring light path [0006] L is the optical path length of the ring light path [0007] Ω is the rotational angular velocity [0008] λ is the laser working wavelength [0009] K is the scaling factor of...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C19/64
Inventor 陈林峰严吉中韩宗虎吕航伟何颖杨洪友王维科马冲泽
Owner FLIGHT AUTOMATIC CONTROL RES INST
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