CN103968821B - Two-way resonance type optical gyroscope - Google Patents
Two-way resonance type optical gyroscope Download PDFInfo
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Abstract
本发明涉及高精度的谐振式光学陀螺,具体为双路谐振式光学陀螺,包括第一环形器CIR1、第二耦合器C2、数据采集模块、第三耦合器C3和第二光电探测器PD2,第一环形器CIR1的第三端口通过光纤和第三耦合器C3的第一输入端连接,第二耦合器C2的第二输出端和第三耦合器C3的第二输入端连接,第三耦合器C3的输出端和第二光电探测器的输入端连接,第二光电探测器的输出端和数据采集模块的采集端口连接;本发明根据频差较小、速度相同的两列同向传播的简谐波叠加可形成拍现象的光学合成原理,提供了双路谐振式光学陀螺,该光学陀螺测频差方便、陀螺内包含的光电器件较少,测得的频差精确,不存在检测闭锁阈值区。
The present invention relates to a high-precision resonant optical gyroscope, specifically a dual-channel resonant optical gyroscope, comprising a first circulator CIR1, a second coupler C2, a data acquisition module, a third coupler C3 and a second photodetector PD2, The third port of the first circulator CIR1 is connected to the first input end of the third coupler C3 through an optical fiber, the second output end of the second coupler C2 is connected to the second input end of the third coupler C3, and the third coupling The output end of the device C3 is connected with the input end of the second photodetector, and the output end of the second photodetector is connected with the acquisition port of the data acquisition module; The simple harmonic superposition can form the optical synthesis principle of the beating phenomenon, and a dual-channel resonant optical gyroscope is provided. The optical gyroscope is convenient to measure the frequency difference, the gyroscope contains fewer photoelectric devices, the measured frequency difference is accurate, and there is no detection lock-up threshold area.
Description
技术领域technical field
本发明涉及高精度的谐振式光学陀螺,具体为双路谐振式光学陀螺。The invention relates to a high-precision resonant optical gyroscope, in particular to a dual-channel resonant optical gyroscope.
背景技术Background technique
谐振式光学陀螺是继微机电陀螺、激光陀螺、干涉式光纤陀螺之后发展起来的一种小体积、低功耗、高精度和高可靠性的新型角速度传感器。在国家深空探测、武器精确制导、北斗导航等重大计划和工程的带动下,高灵敏度、微小型化、高稳定性、抗高过载等特性成为谐振式光学陀螺的发展趋势,而信号的准确检测是实现这些指标的重中之重。Resonant optical gyroscope is a new type of angular velocity sensor with small size, low power consumption, high precision and high reliability developed after MEMS gyroscope, laser gyroscope and interferometric fiber optic gyroscope. Driven by major programs and projects such as national deep space exploration, weapon precision guidance, and Beidou navigation, the characteristics of high sensitivity, miniaturization, high stability, and high overload resistance have become the development trend of resonant optical gyroscopes, and the accuracy of signals Detection is a top priority in achieving these metrics.
谐振式光学陀螺是应用Sagnac效应原理来测量被测载体的旋转角速度,具体为将光学陀螺内部可调谐窄线宽光源(发出光束频率小于1KHz)发出的光束频率通过反馈支路上的反馈控制电路锁定在光纤环形谐振腔的本征透射峰的中心频率上,通过光学陀螺捷联载体转动引起的光电探测幅值变化、并根据此幅值变化进行换算得到光纤环形谐振腔内顺逆两路光束之间的频差,由得到的频差进行转换,从而测得被测运动载体的转动角速度。由于传统的谐振式光学陀螺是通过旋转产生的频差来检测角速度,频差需要由光电探测幅值变化换算得到,而光电探测幅值要通过对光束进行调制和解调得到,因此传统的谐振式光学陀螺内部需要调制器、解调器和一些辅助光电器件,这些器件自身在转动过程中受到振动、白噪声的影响,导致陀螺的检测精度较低,同时这些器件的存在导致陀螺检测存在闭锁阈值区,即陀螺对极慢的或高速的转动信号检测不到,其检测范围受到很大限制。The resonant optical gyroscope uses the Sagnac effect principle to measure the rotational angular velocity of the measured carrier. Specifically, the frequency of the beam emitted by the tunable narrow-linewidth light source (beam frequency less than 1KHz) inside the optical gyroscope is locked by the feedback control circuit on the feedback branch. At the center frequency of the intrinsic transmission peak of the fiber ring resonator, the amplitude change of the photoelectric detection caused by the rotation of the optical gyro strapdown carrier is converted according to the amplitude change to obtain the forward and reverse beams in the fiber ring resonator. The frequency difference between them is converted by the obtained frequency difference, so as to measure the rotational angular velocity of the measured moving carrier. Since the traditional resonant optical gyro detects the angular velocity through the frequency difference generated by rotation, the frequency difference needs to be converted from the change of the photoelectric detection amplitude, and the photoelectric detection amplitude must be obtained by modulating and demodulating the beam, so the traditional resonant The modulator, demodulator and some auxiliary optoelectronic devices are needed inside the optical gyroscope. These devices themselves are affected by vibration and white noise during the rotation process, resulting in low detection accuracy of the gyroscope. At the same time, the existence of these devices leads to a lock-up in the gyroscope detection. In the threshold area, that is, the gyroscope cannot detect extremely slow or high-speed rotation signals, and its detection range is greatly limited.
发明内容Contents of the invention
本发明为了解决现有的谐振式光学陀螺的检测精度低和检测范围受限的问题,提供了双路谐振式光学陀螺。In order to solve the problems of low detection accuracy and limited detection range of the existing resonant optical gyroscope, the invention provides a dual-channel resonant optical gyroscope.
本发明是采用如下的技术方案实现的:双路谐振式光学陀螺,包括隔离准直芯片可调谐光源FL,隔离准直芯片可调谐光源FL的输出端通过光纤和光学隔离器ISO的输入端连接,光学隔离器ISO的输出端通过光纤和第一耦合器C1的输入端连接,第一耦合器C1的第一输出端通过光纤和相位调制器PM的输入端连接,相位调制器PM的输出端通过光纤和第一环形器CIR1的第一端口连接,第一环形器CIR1的第二端口通过光纤和第四耦合器C4的第一端口连接;The present invention is realized by adopting the following technical scheme: a dual-channel resonant optical gyroscope, including an isolation collimation chip tunable light source FL, the output end of the isolation collimation chip tunable light source FL is connected to the input end of the optical isolator ISO through an optical fiber , the output end of the optical isolator ISO is connected to the input end of the first coupler C1 through an optical fiber, the first output end of the first coupler C1 is connected to the input end of the phase modulator PM through an optical fiber, and the output end of the phase modulator PM Connect to the first port of the first circulator CIR1 through an optical fiber, and connect the second port of the first circulator CIR1 to the first port of the fourth coupler C4 through an optical fiber;
第一耦合器C1的第二输出端通过光纤和第二环形器CIR2的第一端口连接,第二环形器CIR2的第二端口通过光纤和第四耦合器C4的第二端口连接,第四耦合器C4的第三端口和第四端口都通过光纤和光纤环形谐振腔FRR的输入端口连接;The second output end of the first coupler C1 is connected to the first port of the second circulator CIR2 through an optical fiber, and the second port of the second circulator CIR2 is connected to the second port of the fourth coupler C4 through an optical fiber, and the fourth coupling The third port and the fourth port of the device C4 are connected to the input port of the optical fiber and the optical fiber ring resonator FRR;
第二环形器CIR2的第三端口通过光纤和第二耦合器C2的输入端连接,第二耦合器C2的第一输出端通过光纤和第一光电探测器PD1的输入端连接,第一光电探测器PD1的输出端通过光纤和锁相放大器LIA的输入端连接,锁相放大器LIA的输出端通过信号线和反馈控制电路FBC的输入端连接,反馈控制电路FBC的输出端和隔离准直芯片可调谐光源FL的反馈端连接;The third port of the second circulator CIR2 is connected to the input end of the second coupler C2 through an optical fiber, the first output end of the second coupler C2 is connected to the input end of the first photodetector PD1 through an optical fiber, and the first photodetector The output end of the PD1 is connected to the input end of the lock-in amplifier LIA through an optical fiber, and the output end of the lock-in amplifier LIA is connected to the input end of the feedback control circuit FBC through a signal line, and the output end of the feedback control circuit FBC and the isolation collimation chip can be The feedback terminal connection of the tuning light source FL;
还包括数据采集处理模块、第三耦合器C3和第二光电探测器PD2,第一环形器CIR1的第三端口通过光纤和第三耦合器C3的第一输入端连接,第二耦合器C2的第二输出端和第三耦合器C3的第二输入端连接,第三耦合器C3的输出端和第二光电探测器PD2的输入端连接,第二光电探测器的输出端和数据采集处理模块的采集端口连接。It also includes a data acquisition and processing module, a third coupler C3 and a second photodetector PD2, the third port of the first circulator CIR1 is connected to the first input end of the third coupler C3 through an optical fiber, and the second coupler C2 The second output terminal is connected to the second input terminal of the third coupler C3, the output terminal of the third coupler C3 is connected to the input terminal of the second photodetector PD2, and the output terminal of the second photodetector is connected to the data acquisition and processing module The collection port connection.
工作时,由隔离准直芯片可调谐光源FL发出的光束经过光学隔离器ISO和第一分束器C1后,被分成两路功率相等、频差为零的两束光,其中一束光经过相位调制器PM和第一环形器CIR1后,由第四耦合器C4进入光纤环形谐振腔FRR,在光纤环形谐振腔FRR内形成逆时针光束,其中另一束光经过第二环形器CIR2后,由第四耦合器C4进入光纤环形谐振腔FRR,在光纤环形谐振腔FRR内形成顺时针光束,逆时针光束在光纤环形谐振腔FRR内绕行一圈,最后通过第四耦合器C4、第二环形器CIR2和第二耦合器C2进入第一光电探测器PD1,然后经锁相放大器LIA、反馈控制电路FBC进入可调谐光源FL的反馈端,对隔离准直芯片可调谐光源FL进行调频,使隔离准直芯片可调谐光源FL输出的光束频率锁定在光纤环形谐振腔FRR的透射谱峰中心频率处;顺时针光束和逆时针光束在光纤环形谐振腔FRR内绕行一圈后在第三耦合器C3处叠加,叠加后的光束进入第二光电探测器PD2进行光电转换,转换后的电信号存储到数据采集模块;顺时针光束和逆时针光束通过第三耦合器C3叠加后,发生拍现象,形成拍频信号,此拍频信号存储到数据采集处理模块内,由数据采集处理模块测得拍频信号的波长,数据采集处理模块再根据公式,可以计算两路光束之间的频率差,根据频率差便可得到被测物的旋转角速度,该光学陀螺内部不需要调制器、解调器和一些辅助器件,在转动过程中不会受到振动、信号白噪声的影响而降低陀螺的检测精度,也不存在检测闭锁阈值区。When working, the light beam emitted by the tunable light source FL of the isolation and collimation chip passes through the optical isolator ISO and the first beam splitter C1, and is divided into two beams of light with equal power and zero frequency difference, one of which passes through After the phase modulator PM and the first circulator CIR1, the fourth coupler C4 enters the fiber ring resonator FRR, and forms a counterclockwise beam in the fiber ring resonator FRR, and another beam of light passes through the second circulator CIR2, The fourth coupler C4 enters the fiber ring resonator FRR, forms a clockwise beam in the fiber ring resonator FRR, and the counterclockwise beam goes around in the fiber ring resonator FRR, and finally passes through the fourth coupler C4, the second The circulator CIR2 and the second coupler C2 enter the first photodetector PD1, and then enter the feedback terminal of the tunable light source FL through the lock-in amplifier LIA and the feedback control circuit FBC, and perform frequency modulation on the tunable light source FL of the isolated collimation chip, so that The frequency of the beam output by the isolated collimation chip tunable light source FL is locked at the center frequency of the transmission spectrum peak of the fiber ring resonator FRR; the clockwise beam and the counterclockwise beam go around in the fiber ring resonator FRR and then couple at the third Superimposed at the coupler C3, the superimposed beam enters the second photodetector PD2 for photoelectric conversion, and the converted electrical signal is stored in the data acquisition module; after the clockwise beam and the counterclockwise beam are superimposed by the third coupler C3, a beating phenomenon occurs , forming a beat frequency signal, the beat frequency signal is stored in the data acquisition and processing module, the wavelength of the beat frequency signal is measured by the data acquisition and processing module, and the data acquisition and processing module then according to the formula , the frequency difference between the two beams can be calculated, and the rotational angular velocity of the measured object can be obtained according to the frequency difference. The optical gyroscope does not need modulators, demodulators and some auxiliary devices inside, and will not be vibrated during the rotation process. , The influence of signal white noise reduces the detection accuracy of the gyroscope, and there is no detection blocking threshold area.
数据采集处理模块内的计算频率差的程序为本领域的技术人员公知的。The program for calculating the frequency difference in the data acquisition and processing module is well known to those skilled in the art.
本发明根据频差较小、速度相同的两列同向传播的简谐波叠加可形成拍现象的光学合成原理,提供了简便的双路谐振式光学陀螺,该双路谐振式光学陀螺测频差方便、陀螺内包含的光电器件较少,测得的频差精确,不存在检测闭锁阈值区,解决了现有的谐振式光学陀螺灵敏度不高和检测范围受限的问题。The present invention provides a simple dual-channel resonant optical gyroscope based on the principle of optical synthesis that the superposition of simple harmonic waves propagating in the same direction with small frequency differences and the same speed can form a beating phenomenon. The frequency difference is convenient, the gyroscope contains fewer photoelectric devices, the measured frequency difference is accurate, and there is no detection blocking threshold area, which solves the problems of low sensitivity and limited detection range of the existing resonant optical gyroscope.
附图说明Description of drawings
图1为本发明的结构示意图。Fig. 1 is a structural schematic diagram of the present invention.
图2为示波器检测到的拍频信号的波形图。Figure 2 is a waveform diagram of the beat frequency signal detected by the oscilloscope.
图3为计算得到的频差示意图。Fig. 3 is a schematic diagram of the calculated frequency difference.
具体实施方式detailed description
双路谐振式光学陀螺,包括隔离准直芯片可调谐光源FL,隔离准直芯片可调谐光源FL的输出端通过光纤和光学隔离器ISO的输入端连接,光学隔离器ISO的输出端通过光纤和第一耦合器C1的输入端连接,第一耦合器C1的第一输出端通过光纤和相位调制器PM的输入端连接,相位调制器PM的输出端通过光纤和第一环形器CIR1的第一端口连接,第一环形器CIR1的第二端口通过光纤和第四耦合器C4的第一端口连接;Dual-channel resonant optical gyro, including an isolated collimation chip tunable light source FL, the output end of the isolated collimation chip tunable light source FL is connected to the input end of the optical isolator ISO through an optical fiber, and the output end of the optical isolator ISO is connected through an optical fiber and The input end of the first coupler C1 is connected, the first output end of the first coupler C1 is connected to the input end of the phase modulator PM through an optical fiber, and the output end of the phase modulator PM is connected to the first end of the first circulator CIR1 through an optical fiber. Port connection, the second port of the first circulator CIR1 is connected to the first port of the fourth coupler C4 through an optical fiber;
第一耦合器C1的第二输出端通过光纤和第二环形器CIR2的第一端口连接,第二环形器CIR2的第二端口通过光纤和第四耦合器C4的第二端口连接,第四耦合器C4的第三端口和第四端口都通过光纤和光纤环形谐振腔FRR的输入端口连接;The second output end of the first coupler C1 is connected to the first port of the second circulator CIR2 through an optical fiber, and the second port of the second circulator CIR2 is connected to the second port of the fourth coupler C4 through an optical fiber, and the fourth coupling The third port and the fourth port of the device C4 are connected to the input port of the optical fiber and the optical fiber ring resonator FRR;
第二环形器CIR2的第三端口通过光纤和第二耦合器C2的输入端连接,第二耦合器C2的第一输出端通过光纤和第一光电探测器PD1的输入端连接,第一光电探测器PD1的输出端通过光纤和锁相放大器LIA的输入端连接,锁相放大器LIA的输出端通过信号线和反馈控制电路FBC的输入端连接,反馈控制电路FBC的输出端和隔离准直芯片可调谐光源FL的反馈端连接;The third port of the second circulator CIR2 is connected to the input end of the second coupler C2 through an optical fiber, the first output end of the second coupler C2 is connected to the input end of the first photodetector PD1 through an optical fiber, and the first photodetector The output end of the PD1 is connected to the input end of the lock-in amplifier LIA through an optical fiber, and the output end of the lock-in amplifier LIA is connected to the input end of the feedback control circuit FBC through a signal line, and the output end of the feedback control circuit FBC and the isolation collimation chip can be The feedback terminal connection of the tuning light source FL;
还包括数据采集处理模块、第三耦合器C3和第二光电探测器PD2,第一环形器CIR1的第三端口通过光纤和第三耦合器C3的第一输入端连接,第二耦合器C2的第二输出端和第三耦合器C3的第二输入端连接,第三耦合器C3的输出端和第二光电探测器的输入端连接,第二光电探测器的输出端和数据采集处理模块的采集端口连接。It also includes a data acquisition and processing module, a third coupler C3 and a second photodetector PD2, the third port of the first circulator CIR1 is connected to the first input end of the third coupler C3 through an optical fiber, and the second coupler C2 The second output terminal is connected to the second input terminal of the third coupler C3, the output terminal of the third coupler C3 is connected to the input terminal of the second photodetector, and the output terminal of the second photodetector is connected to the data acquisition processing module. Acquisition port connection.
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