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CN109556591A - A kind of passive type lasergyro based on super stabilized laser - Google Patents

A kind of passive type lasergyro based on super stabilized laser Download PDF

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Publication number
CN109556591A
CN109556591A CN201811403103.7A CN201811403103A CN109556591A CN 109556591 A CN109556591 A CN 109556591A CN 201811403103 A CN201811403103 A CN 201811403103A CN 109556591 A CN109556591 A CN 109556591A
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laser
frequency
signal
cavity
transmission unit
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CN109556591B (en
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张洁
柳奎
张风雷
陆泽晃
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Huazhong University of Science and Technology
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Huazhong University of Science and Technology
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/58Turn-sensitive devices without moving masses
    • G01C19/64Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
    • G01C19/66Ring laser gyrometers
    • G01C19/661Ring laser gyrometers details

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  • Engineering & Computer Science (AREA)
  • Optics & Photonics (AREA)
  • Electromagnetism (AREA)
  • Power Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Gyroscopes (AREA)
  • Lasers (AREA)

Abstract

本发明公开了一种基于超稳激光的被动式激光陀螺仪,包括超稳激光光源装置、高Q值环形腔干涉仪装置和拍频探测装置,激光器输出激光频率锁定至超稳法珀腔谐振峰,同时锁定至链接到原子频标的飞秒光梳,获得兼具短稳与长稳的超稳激光源;环形腔的周长锁定至沿逆时针方向注入的超稳激光源频率上,沿顺时针方向注入的激光频率锁定到腔同一谐振峰上;拍频探测装置探测腔内两个方向溢出光的拍频得到Sagnac信号,通过此信号确定旋转角速度。本发明通过利用超稳激光作为被动式激光陀螺仪注入光源,改善激光陀螺仪干涉信噪比,同时使得陀螺仪的标度因子稳定性可以得到提高,从而提高整个陀螺仪系统的稳定性,延长积分平均时间,以获得更好的转动测量分辨率。

The invention discloses a passive laser gyroscope based on an ultra-stable laser, comprising an ultra-stable laser light source device, a high-Q value ring cavity interferometer device and a beat frequency detection device. , at the same time locked to the femtosecond optical comb linked to the atomic frequency standard to obtain an ultra-stable laser source with both short and long stability; the circumference of the ring cavity is locked to the frequency of the ultra-stable laser source injected in the counterclockwise direction, and the The frequency of the laser injected in the clockwise direction is locked to the same resonance peak of the cavity; the beat frequency detection device detects the beat frequencies of the overflowing light in two directions in the cavity to obtain the Sagnac signal, and the rotation angular velocity is determined by this signal. The invention improves the interference signal-to-noise ratio of the laser gyroscope by using the ultra-stable laser as the passive laser gyroscope injection light source, and at the same time, the stability of the scale factor of the gyroscope can be improved, thereby improving the stability of the whole gyroscope system and prolonging the integral Averaging time for better rotational measurement resolution.

Description

A kind of passive type lasergyro based on super stabilized laser
Technical field
The invention belongs to lasergyro fields, swash more particularly, to a kind of passive type based on super stabilized laser technology Optical gyroscope.
Background technique
Lasergyro is used for inertial navigation, geophysics, basis due to its excellent slewing rate measurement performance The fields such as physics.In past 40 years, lasergyro has become inertial navigation and precision rotation fields of measurement is most important Instrument, due to its high resolution, stability is good, dynamic range is wide and the favor by scientific research circle and industry researcher. Lasergyro is based on Sagnac effect, is proposed in 1913 by French scientist Sagnac, in an annular chamber, if being There is rotation in the propagation plane of light in system, then the reality that the light propagated clockwise is passed by with the light counterclockwise propagated Light path is unequal, if two-beam resonates with the same resonance peak of annular chamber simultaneously, the difference of their resonant frequency with The relationship of angular velocity of rotation can indicate are as follows:Wherein fsagnac is the both direction resonance that we measure The difference on the frequency of laser, also referred to as Sagnac frequency, whereinReferred to as scale factor, A are the circular areas of annular chamber, and λ is sharp The wavelength of light, P are the perimeters of annular chamber, and Ω is the angular velocity of rotation of annular chamber.As can be seen that the circular area of lasergyro Bigger, scale factor is bigger, and measurement sensitivity is higher.
Existing gyroscope is largely active laser gyroscope, i.e., is done by the loop laser that four anti-hysteroscopes of height are constituted It is full of He-Ne gas gain medium inside interferometer, themselves is exactly an active ring laser, suitable/counterclockwise The frequency difference of the laser output of direction resonance is Sagnac frequency.This active laser designing gyroscope thought is relatively easy and straight It connects, limiting factor mostlys come from two aspects at present: one is constrained to the disturbance of spontaneous emission noise and intracavitary medium;Second is that Dithered and other Frequency-Biasing Techniques for overcoming lasergyro frequency latch-up phenomenon can lose the stabilization of lasergyro Property.
Passive lasergyro laser source is located at outside annular chamber, can effectively avoid spontaneous emission noise and intracavitary medium Disturbance, using the method for external modulation also it is possible to prevente effectively from the frequency latch-up phenomenon being widely present in lasergyro.But by Dynamic formula gyroscope is generally limited by the stability of injection laser source and the stability of itself annular chamber, can neither obtain good rotation Tarnsition velocity detectivity, can not obtain the very long time of integration averagely obtains good angular velocity of rotation resolution ratio. In order to solve this problem, patent document CN103047979 B provide it is a kind of using feedback system by the center of laser signal Frequency Locking is in Fabry Perot chamber resonance frequency, to realize that laser aid output laser linewidth narrows and laser frequency Stablize, improves the measurement accuracy and sensitivity of the angular velocity of rotation of lasergyro, but it does not solve Fabry Perot chamber Resonance frequency long term drift problem, the passive type lasergyro integral mean time can be very limited, and in addition to this it does not have yet Provide passive type lasergyro stabilization or post-processing scheme.
Summary of the invention
Aiming at the above defects or improvement requirements of the prior art, the present invention provides a kind of passive types based on super stabilized laser Lasergyro, its object is to solve in existing passive type lasergyro due to injection laser noise and Gyroscopic stabilization Property difference caused by the not high enough problem of detection resolution, pass through and improve passive type lasergyro and inject laser source stability and mark Factor stability is spent, so that laser linewidth is much smaller than annular chamber line width, lasergyro interference signal signal-to-noise ratio is improved, mentions simultaneously It is the rotated detection sensitivity of high lasergyro and the longtime running time of integration, final to improve rotated detection resolution ratio.
To achieve the above object, according to one aspect of the present invention, it is sharp to provide a kind of passive type based on super stabilized laser Optical gyroscope, comprising: super stabilized laser light supply apparatus, high q-factor annular chamber interferometer and beat frequency detection device;It is described super steady sharp Radiant device includes: laser aid, Fabry Perot chamber device, femtosecond light comb device and atomic frequency standard device;Laser aid Laser signal, laser letter are provided to the Fabry Perot chamber device, femtosecond light comb device and annular chamber interferometer respectively Number frequency simultaneously be locked to the Fabry Perot chamber and femtosecond light comb device, at the same time, femtosecond light comb device by itself Repetition rate and zero bias Frequency Locking are to atomic frequency standard device, so that laser aid final output laser signal frequency has both simultaneously The short-term stability of Fabry Perot chamber and the long-time stability of atomic frequency standard;The high q-factor annular chamber interferometer is used to Passive type lasergyro optical interference circuit is constructed, the laser aid exports laser with short-term stabilization for a long time through overfrequency later Signal divides two-way, respectively in the counterclockwise direction with inject the annular chamber device clockwise;Injection swashs in the counterclockwise direction The annular chamber device resonance frequency is locked to laser as length standard, by the long frequency locker of the chamber by optical signal In signal frequency, laser signal is injected along clockwise direction and injects the annular chamber device and laser signal frequency is locked to institute It states in annular chamber device resonance frequency;Beat frequency detection device is divided within the high q-factor annular chamber interferometer for detecting The difference Sagnac signal for the laser signal frequency that do not propagate in the counterclockwise direction with clockwise direction determines whole device with this Angular velocity of rotation.
Wherein, atomic frequency standard device 104 can use stable a reference source to realize, such as in super stabilized laser light supply apparatus 100 Rubidium clock, caesium clock, hydrogen clock, opctical frequency standard etc.;The group of femtosecond light comb device 103 and frequency marking device 104 in super stabilized laser light supply apparatus 100 Conjunction can be replaced with iodine molecule, rubidium atom, Cs atom frequency stabilization system.
Further, passive type lasergyro further include: first laser transmission unit, the first feedback unit, second Laser transmission unit and the second feedback unit;The first input end of second laser transmission unit is connected to the defeated of femtosecond light comb device Outlet, the second input terminal of second laser transmission unit are connected to the output end of laser aid, the input terminal of the second feedback unit It is connected to the output end of second laser transmission unit, the first input end that the output end of the second feedback unit is connected to;First swashs The input terminal of optical transmission unit is connected to the output end of laser aid, the input/output terminal of first laser transmission unit and connection, The input terminal of first feedback unit is connected to the output end of first laser transmission unit, and the output end of the first feedback unit is connected to The second input terminal;First laser transmission unit is used for the laser signal transmission that exports laser aid to the Fabry Perot Chamber;First feedback unit is used to the laser signal frequency that laser aid exports being locked to the Fabry Perot chamber;Second swashs Optical transmission unit is used for the laser signal transmission that exports laser aid to the femtosecond light comb device;Second feedback unit is used for The laser signal frequency that laser aid exports is locked to the femtosecond light comb device.
Further, the frequency of the laser signal of laser aid output by Fabry Perot chamber device and is linked to atom The femtosecond light comb device of frequency marking is stablized.
Further, the frequency short-term stability of the laser signal of laser aid output is stablized by Fabry Perot chamber, The beam of laser that laser signal is reflected through the second spectroscope by the first electrooptic modulator phase-modulation, after it is anti-by optoisolator Fa-Po cavity is injected, which is reflected after interacting with Fa-Po cavity, the detectable signal at the first photodetector, gained Laser aid is fed back to after the first servo amplifier after error signal demodulation, by laser aid output laser signal frequency lock Determine onto Fa-Po cavity resonance peak, obtains the superior short-term stability of Fa-Po cavity;The frequency of the laser signal of the laser aid output Rate long-time stability are stablized by the femtosecond light comb for being linked to atomic frequency standard, and laser signal is reflected a branch of sharp through the first spectroscope The shoot laser signal of light and the femtosecond light comb device being linked on atomic frequency standard device synthesizes a branch of after third spectroscope Laser, detects beat signal on the second photodetector, and gained signal feeds back to laser dress after the second servo amplifier It sets, laser aid output laser signal frequency is locked on the femtosecond light comb device for being linked to atomic frequency standard device, so that swashing Electro-optical device is provided with the long-time stability of atomic frequency standard.
Further, high q-factor annular chamber interferometer includes: gyro laser preparatory unit, third laser transmission list Member, the 4th laser transmission unit, annular chamber, third feedback unit, the 4th feedback unit;First laser signal connects gyro laser quasi The input terminal of standby unit, the first output end of gyro laser preparatory unit are connected to the input terminal of third laser transmission unit, top The second output terminal of spiral shell laser preparatory unit is connected to the input terminal of the 4th laser transmission unit, third laser transmission unit it is defeated Enter output end to connect with annular chamber, the input/output terminal of the 4th laser transmission unit is connect with annular chamber;Third feedback unit Input terminal is connected to the second output terminal of the 4th laser transmission unit, and the input terminal of the 4th feedback unit is connected to third laser The second output terminal of defeated unit;The output end of third feedback unit is connected to another input terminal of annular chamber, the 4th feedback unit Output end be connected to another input terminal of the 4th laser transmission unit;Gyro laser preparatory unit is used for first laser signal It carries out phase-modulation and is divided into two beams;Third laser transmission unit is used for the laser signal for exporting gyro laser preparatory unit It transmits and is injected into the annular chamber;Another laser that 4th laser transmission unit is used to export gyro laser preparatory unit is believed Number transmit and be injected into the annular chamber;Annular chamber respectively generates resonance and interferes for two beams injection laser signal;Third is anti- The error signal servo feedback between laser signal that feedback unit is used to inject by annular chamber resonance peak and in the counterclockwise direction is extremely Piezoelectric ceramics;The error between laser signal that 4th feedback unit is used to inject by annular chamber resonance peak and along clockwise direction Signal servo feedback is to second sound-optic modulator.
Further, the long super stabilized laser by injecting in the counterclockwise direction of the chamber of annular chamber is stablized: in the counterclockwise direction Inject first laser signal and carry out phase-modulation by the second electrooptic modulator, generate after phase-modulation laser carrier signal and The sideband signals that two amplitude is equal, amplitude is opposite, sideband directly by annular cavity reflection, after carrier wave and chamber interaction with sideband Third photodetector is reflected by second faraday isolator together, by third photodetector exploring laser light carrier frequency The mismatching angle of rate and annular chamber resonance peak, demodulation obtain error signal, and final feedback arrives piezoelectric ceramics, to push the 4th high reflection Rate hysteroscope, the chamber for changing annular chamber is long, and the chamber length of annular chamber is locked in the frequency of injection laser signal counterclockwise.
Further, the super stabilized laser signal injected along clockwise direction passes through second sound-optic modulator, Frequency Locking Onto the chamber length of the annular chamber, in which: inject laser signal sideband along clockwise direction by annular cavity reflection, carrier wave and chamber phase The 4th photodetector is reflected by first faraday isolator together with sideband after interaction, by the 4th photodetector The mismatching angle of exploring laser light carrier frequency and annular chamber resonance peak, demodulation obtain error signal, final feedback to the second acousto-optic tune Device processed drives voltage controlled oscillator, to change the modulating frequency f of second sound-optic modulator2, so that injecting laser along clockwise direction Frequency and annular chamber resonance, will inject along clockwise direction the Frequency Locking of laser to annular chamber chamber it is long on.
Further, Sagnac signal both can use the modulation frequency of first sound-optic modulator and second sound-optic modulator The difference of rate obtains, and also can use and obtains from the spilling photo-beat frequency detection in latter two direction of chamber.
In general, through the invention it is contemplated above technical scheme is compared with the prior art, have it is following beneficial to effect Fruit:
(1) present invention is stabilized to super steady Fabry Perot chamber and chain by the way that passive type lasergyro is injected light source simultaneously It is connected in the femtosecond light comb of hydrogen clock, so that passive type lasergyro injection light source is had both short-term stability and long-time stability, make It obtains laser linewidth and is much smaller than annular chamber line width, improve lasergyro interference signal signal-to-noise ratio, improve passive type lasergyro 2-3 order of magnitude of rotated detection sensitivity, while promoting the detection resolution under the long time of integration.
(2) piezoelectric ceramics is loaded on annular chamber wherein one side hysteroscope, is locked to super stabilized laser source using by annular chamber Method improves the scalefactor stability of lasergyro.
Detailed description of the invention
Fig. 1 is a kind of overall construction drawing of the passive type lasergyro the present invention is based on super stabilized laser;
Fig. 2 is the schematic diagram of a specific embodiment of super stabilized laser light supply apparatus in the present invention;
Fig. 3 is a specific embodiment schematic diagram of high q-factor annular chamber interferometer in the present invention;
Fig. 4 is a specific embodiment schematic diagram of beat frequency detection device in the present invention.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to the accompanying drawings and embodiments, right The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and It is not used in the restriction present invention.As long as in addition, technical characteristic involved in the various embodiments of the present invention described below Not constituting a conflict with each other can be combined with each other.
The present invention provides a kind of passive type lasergyro based on super stabilized laser, Fig. 1 is a kind of totality of the invention Structure chart, mainly by super stabilized laser light supply apparatus 100, high q-factor annular chamber interferometer 200 and beat frequency detection device 300.Its In super stabilized laser light supply apparatus 100 include: laser aid 101, it is Fabry Perot chamber device 102, femtosecond light comb device 103, former Sub- frequency marking device 104.
Wherein, a part output that laser aid 101 exports laser signal is interacted therewith to Fa-Po cavity device 102 After obtain error signal, error signal feeds back to laser aid 101, and the output laser signal frequency of laser aid 101 is locked Onto the Fa-Po cavity resonance peak in Fa-Po cavity device 102, the output laser signal frequency to stabilized lasers device 101 is steady in short term It is qualitative;
The another part that separates that laser aid 101 exports laser signal is exported to femtosecond light comb device 103, femtosecond light comb dress It sets 103 and has been locked to atomic frequency standard device 104 using the characteristic and device of itself, have the stability of hydrogen clock, laser Device 101 is output to the laser signal of femtosecond light comb device 103 and the output light action of femtosecond light comb device 103, obtained mistake Difference signal feeds back to laser aid 101, the output laser signal frequency long-time stability to stabilized lasers device 101;
Specific implementation example according to the present invention, Fa-Po cavity device 102 can be used ultra-high stable Fa-Po cavity, be locked to The laser signal short-term stability Alan deviation of Fa-Po cavity can be better than 10-12, it is preferable that 10 can be better than-13、10-14、10-15、10-16、10-17Or 10-18
Hydrogen clock can be used as atomic frequency standard device 104, as a long time surely in specific implementation example according to the present invention Determine reference source, be linked to hydrogen clock using femtosecond light comb device 103, is locked to the laser signal long-time stability Alan of femtosecond light comb Deviation can be better than 10-12, it is preferable that 10 can be better than-13、10-14、10-15、10-16;Preferably, other reference sources, such as iodine can be used Molecule frequency marking, light clock etc., it is preferable that long-time stability can be better than 10-13、10-14、10-15、10-16、10-17、10-18Or 10-19
Fig. 2 is the schematic diagram of a specific embodiment of super stabilized laser light supply apparatus in the present invention.Attached drawing of the invention In, heavy line indicates optical path, thick dashed line indication circuit.Super stabilized laser light supply apparatus 100 includes: laser aid 101, Fabry amber Sieve chamber device 102, femtosecond light comb device 103, atomic frequency standard device 104 and first laser transmission unit 105, the first feedback First 106, second laser transmission unit 107, the second feedback unit 108;Laser aid 101 is used to provide laser letter to whole system Number, Fabry Perot chamber device 102 is used for the short-term stability reference source of laser signal, and femtosecond light comb device 103 is sharp for linking Optical signal and atomic frequency standard output signal, atomic frequency standard device 104 are used for the short-term stability reference source of laser signal, first laser The laser signal transmission that transmission unit 105 is used to export laser aid 101 to the Fabry Perot chamber 102, first is fed back Unit 106 is used to the laser signal frequency that laser aid 101 exports being locked to the Fabry Perot chamber 102, second laser The laser signal transmission that transmission unit 107 is used to export laser aid 101 to the femtosecond light comb device 103, second is fed back Unit 108 is used to the laser signal frequency that laser aid 101 exports being locked to the femtosecond light comb device 103.
Wherein, laser aid 101 includes: laser 1011 and be arranged on the emitting light path of laser 1011 first point Light microscopic 1012;Laser 1011 is used to laser being divided into two beams for emitting original laser signal, the first spectroscope 1012;
First laser transmission unit 105 includes: the second spectroscope 1051, the first electrooptic modulator 1052, optoisolator 1053;By laser aid 101 be emitted wherein all the way laser signal by 1051 part of the second spectroscope reflection after passed sequentially through First electrooptic modulator 1052 and optoisolator 1053 reach enamel amber chamber 102;Second spectroscope 1051 is for part reflection and thoroughly Laser signal is penetrated, the first electrooptic modulator 1052 is used to carry out phase-modulation to laser signal, and optoisolator 1053 will be for that will swash Optical signal reflexes to enamel amber chamber 102 and receives the laser signal of the return of enamel amber chamber 102.
First feedback unit 106 includes: the first photodetector 1061 and the first servo amplifier 1062;First photoelectricity is visited Device 1061 is surveyed to be placed in after optoisolator 1053 for detecting the laser signal returned from enamel amber chamber 102, the first servo amplifier 1062 between the first photodetector 1061 and laser 1011, for this short steady loop error signal demodulation, put Greatly and servo feedback.
Second laser transmission unit 107 includes: third spectroscope 1071;Third spectroscope 1071 is placed in laser aid 101 Between femtosecond light comb 103, the transmission of the laser signal and 103 output signal of femtosecond light comb that export for laser aid 101 is believed Number close beam.
Second feedback unit 108 includes: the second photodetector 1081 and the second servo amplifier 1082;Second photoelectricity is visited It surveys after device 1081 is placed in third spectroscope 1071 and is used for the laser signal and femtosecond light comb 103 that exploring laser light device 101 exports The beat signal of output signal, the second servo amplifier 1082 then in the second photodetector 1081 and laser 1011 it Between, the demodulation, amplification and servo feedback of steady loop error signal are grown for this.
Wherein the shoot laser signal of laser 1011 passes through the first spectroscope 1012, gets beam of laser through the second light splitting It, should by being reflected into Fa-Po cavity 102 by optoisolator 1053 after 1052 phase-modulation of the first electrooptic modulator after the reflection of mirror 1051 Laser signal is reflected after interacting with Fa-Po cavity 102, the detectable signal at the first photodetector 1061, errors letter Number demodulation after feed back to laser 1011 after the first servo amplifier 1062, by laser aid 101 export laser signal frequency Rate is locked on 102 resonance peak of Fa-Po cavity, obtains the superior short-term stability of Fa-Po cavity 102;Get another beam of laser and chain The shoot laser signal for the femtosecond light comb device 103 being connected on hydrogen clock 104 closes beam after third spectroscope 1071, in the second light Beat signal is detected on electric explorer 1081, gained signal feeds back to laser 1011 after the second servo amplifier 1082, The output laser signal frequency of laser aid 101 is locked on the femtosecond light comb device 103 for being linked to hydrogen clock 104, so that laser Device 101 is provided with the long-time stability of hydrogen clock 104;Two-way feeds back while carrying out, and realizes laser aid 101 and exports laser letter Number long run frequency is stable and short-term frequency stability.
First laser signal is denoted as by the laser signal that the second spectroscope 1051 transmits.First laser signal is supplied to high Q It is worth annular chamber interferometer 200, is used as passive type lasergyro light source.
In this specific embodiment, laser can be Nd:YAG solid state laser.
According to another embodiment of the present invention, laser can be optical fiber laser.
According to another embodiment of the present invention, hydrogen clock can be replaced by other atomic clocks or light clock or other frequency markings.
Fig. 3 is a specific embodiment schematic diagram of high q-factor annular chamber interferometer 200 in the present invention.Of the invention In attached drawing, heavy line indicates optical path, thick dashed line indication circuit.High q-factor annular chamber interferometer 200 includes: gyro laser quasi Standby unit 201, third laser transmission unit 202, the 4th laser transmission unit 203, annular chamber 204, third feedback unit 205, 4th feedback unit 206.Gyro laser preparatory unit 201 is used to first laser signal carrying out phase-modulation and is divided into two Beam, third laser transmission unit 202 are used for laser signal transmission that gyro laser preparatory unit 201 exports and are injected into described Annular chamber 204, the 4th laser transmission unit 203 are used for another laser signal transmission for exporting gyro laser preparatory unit 201 And it is injected into the annular chamber 204, annular chamber 204 respectively generates resonance and interferes for two beams injection laser signal, and third is anti- The error signal servo between laser signal that feedback unit 205 is used to inject by 204 resonance peak of annular chamber and in the counterclockwise direction Piezoelectric ceramics 2045 is fed back to, the 4th feedback unit 206 is used to swash 204 resonance peak of annular chamber with what is injected along clockwise direction Error signal servo feedback between optical signal is to second sound-optic modulator 2031.
Wherein, gyro laser preparatory unit 201 includes: the second electrooptic modulator 2011 and first laser signal is arranged in Half-wave plate 2012 and polarization splitting prism 2013 on emitting light path;Second electrooptic modulator 2011 is for first laser signal Phase-modulation, half-wave plate 2012 are used to adjust the polarization state of laser signal, and polarization splitting prism 2013 is for believing first laser Number it is divided into two parts;
Third laser transmission unit 202 includes: first sound-optic modulator 2021, the first reflecting mirror 2022, the first faraday Isolator 2023;By gyro laser preparatory unit 201 be emitted wherein laser signal passes sequentially through first sound-optic modulator all the way 2021, the first reflecting mirror 2022 and the first faraday isolator 2023 reach annular chamber 204;First sound-optic modulator 2021 is used In carrying out shift frequency to the laser signal that will inject annular chamber in the counterclockwise direction, the first reflecting mirror 2022 is used for laser signal Directive property is adjusted, and the first faraday isolator 2023 returns along clockwise direction for being isolated and extracting annular chamber 204 The laser signal of propagation.
4th laser transmission unit 203 includes: second sound-optic modulator 2031 and the second reflecting mirror 2032, the second faraday Isolator 2033;Second sound-optic modulator is passed sequentially through by the another way laser signal that gyro laser preparatory unit 201 is emitted 2031, the second reflecting mirror 2032 and the second faraday isolator 2033 reach annular chamber 204;Second sound-optic modulator 2031 is used In carrying out shift frequency to the laser signal that will inject annular chamber along clockwise clockwise, the second reflecting mirror 2032 is used for laser Signal directive property is adjusted, the second faraday isolator 2033 be used for be isolated and extract annular chamber 204 return along counterclockwise The laser signal that direction is propagated.
Annular chamber 204 includes: the first high reflectance hysteroscope 2041, the second high reflectance hysteroscope 2042, third high reflectance Hysteroscope 2043, the 4th high reflectance hysteroscope 2044, piezoelectric ceramics 2045;Wherein the first high reflectance hysteroscope 2041, second is high anti- It penetrates rate hysteroscope 2042, third high reflectance hysteroscope 2043, the 4th high reflectance hysteroscope 2044 to be arranged successively, constitutes a closure Square annular chamber 204 respectively generates resonance to two beams injection laser signal and interferes, and piezoelectric ceramics 2045 is arranged the 4th It is used to that hysteroscope is pushed to change 204 chamber of annular chamber after high reflectance hysteroscope 2044 long.
Third feedback unit 205 includes: third photodetector 2051, third servo amplifier 2052;Third photoelectricity is visited Device 2051 is surveyed to be placed in after the second faraday isolator 2033 for detecting the propagation in the counterclockwise direction returned from annular chamber 204 Laser signal, third servo amplifier 2052 is between third photodetector 2051 and piezoelectric ceramics 2045, is used for this Demodulation, amplification and the servo feedback of the long locked loop error signal of chamber.
4th feedback unit 206 includes: the 4th photodetector 2061, the 4th servo amplifier 2062, the second acousto-optic tune Device processed drives voltage controlled oscillator 2063;4th photodetector 2061 is placed in after the first faraday isolator 2023, Zhi Houyi The 4th servo amplifier 2062 of secondary connection, second sound-optic modulator drive voltage controlled oscillator 2063, second sound-optic modulator 2031; 4th photodetector 2061 is used to detect the laser signal propagated along clockwise direction returned from annular chamber 204, and the 4th watches Demodulation, amplification and servo feedback of the amplifier 2062 to this frequency locked loop error signal are taken, second sound-optic modulator drives Dynamic voltage controlled oscillator 2063 is used to provide driving signal to second sound-optic modulator 2031, and second sound-optic modulator 2031 is for passing through Cross the shift frequency of its laser signal.
The first laser signal wherein provided by super stabilized laser light supply apparatus 100 is carried out by the second electrooptic modulator 2011 Phase-modulation generates the carrier signal and two sideband signals that amplitude is equal, amplitude is opposite of laser, sideband letter after phase-modulation Number depend on the modulating frequency of electrooptic modulator 201 with the frequency interval of carrier signal, it is phase modulated after first laser letter Number two-way laser signal is divided by half-wave plate 2012 and polarization splitting prism 2013, it is anti-by the polarization splitting prism 2013 The laser signal penetrated then passes through first sound-optic modulator shift frequency f1, then pass through the first reflecting mirror 2022 and the first faraday every From device 2023, inject in the counterclockwise direction high anti-by the first high reflectance hysteroscope 2041, the second high reflectance hysteroscope 2042, third Penetrate the annular chamber 204 that rate hysteroscope 2043, the 4th high reflectance hysteroscope 2044 and piezoelectric ceramics 2045 are constituted;By the polarization spectro The laser signal that prism 2013 transmits then passes through second sound-optic modulator shift frequency f2Afterwards, then pass through the second reflecting mirror 2032 and the Two faraday isolators 2033 inject annular chamber 204 along clockwise direction.
Wherein, the first faraday isolator 2023 and the second faraday isolator 2033 are for extracting side clockwise respectively Laser signal and counter clockwise direction injection laser signal of the laser through annular cavity reflection to injection laser through annular cavity reflection.Institute It is better than 60dB with faraday isolator isolation, it is preferable that 90dB can be better than.
Wherein, injection laser signal sideband is directly by annular cavity reflection in the counterclockwise direction, after carrier wave interacts with chamber Third photodetector 2051 is reflected by second faraday isolator 2033 together with sideband, by third photodetector The mismatching angle of 2051 exploring laser light carrier frequencies and annular chamber resonance peak, demodulation obtain error signal, and final feedback is made pottery to piezoelectricity Porcelain 2045, to push the 4th high reflectance hysteroscope 2044, the chamber for changing annular chamber is long, is thus locked to the chamber length of annular chamber In the frequency of injection laser signal counterclockwise.
Assuming that the frequency of first laser signal is ν0, then the laser frequency propagated in the counterclockwise direction in annular chamber are as follows: νccw0+f1;Wherein, injection laser signal sideband is equally interacted by annular cavity reflection, carrier wave and chamber along clockwise direction The 4th photodetector 2061 is reflected by first faraday isolator 2023 together with sideband afterwards, by the 4th photodetection The mismatching angle of device 2061 exploring laser light carrier frequency and annular chamber resonance peak, demodulation obtain error signal, final feedback to second Acousto-optic modulator drives voltage controlled oscillator 2063, to change the modulating frequency f of second sound-optic modulator2, so that along side clockwise It resonates to the frequency and annular chamber of injection laser, thus by the Frequency Locking of injection laser along clockwise direction to annular chamber chamber In length.Assuming that the frequency of first laser signal is ν0, then the laser frequency propagated along clockwise direction in annular chamber are as follows: νcw0+f2;First sound-optic modulator 2021 and second sound-optic modulator 2031 are the modulation device of same model, shift frequency direction Unanimously, so two beam laser all resonate with the same longitudinal mode of annular chamber, due to annular chamber rotation there are them to generate Frequency shift (FS) is denoted as fsagnac, can indicate are as follows: fsagnac=f1-f2, i.e. first sound-optic modulator 2021 and the second acousto-optic modulation The difference of 2031 modulating frequency of device is equal to Sagnac frequency.
Fig. 4 is a specific embodiment schematic diagram of beat frequency detection device in the present invention.It include: reflecting mirror 301, reflecting mirror 302, beam cementing prism 303 and the 5th photodetector 304;The setting of reflecting mirror 301 is in third high reflectance hysteroscope 2043 and closes beam To reflect and adjust spilling laser signal in the counterclockwise direction between prism 303, reflecting mirror 302 is arranged in third high reflection To reflect and adjust spilling laser signal along clockwise direction, beam cementing prism between rate hysteroscope 2043 and beam cementing prism 303 303 overflow the conjunction beam of laser signal for intracavitary both direction, and the 5th photodetector 304 being placed in after beam cementing prism is used for Intracavitary both direction overflows the beat frequency detection of laser signal.Its beat frequency is exactly the Sagnac frequency that we need to detect.
The present invention proposes one kind and is based on for detectivity and detection resolution in current large laser gyroscope The passive type lasergyro of super stabilized laser can further promote the detectivity of passive lasergyro, and to mark The available raising of factor stability is spent, to improve the stability of entire gyroscope system, long-time integration is obtained and averagely imitates Fruit, to obtain better rotation measuring resolution ratio.
As it will be easily appreciated by one skilled in the art that the foregoing is merely illustrative of the preferred embodiments of the present invention, not to The limitation present invention, any modifications, equivalent substitutions and improvements made within the spirit and principles of the present invention should all include Within protection scope of the present invention.

Claims (8)

1.一种基于超稳激光的被动式激光陀螺仪,其特征在于,所述被动式激光陀螺包括:超稳激光光源装置(100)、高Q值环形腔干涉仪装置(200)和拍频探测装置(300);1. a passive laser gyroscope based on ultra-stable laser, is characterized in that, described passive laser gyro comprises: ultra-stable laser light source device (100), high-Q value ring cavity interferometer device (200) and beat frequency detection device (300); 所述超稳激光光源装置包括:激光装置(101)、法布里珀罗腔装置(102)、飞秒光梳装置(103)和原子频标装置(104);The ultra-stable laser light source device includes: a laser device (101), a Fabry-Perot cavity device (102), a femtosecond optical comb device (103) and an atomic frequency standard device (104); 所述激光装置(101)分别向所述法布里珀罗腔装置(102)、飞秒光梳装置(103)和环形腔干涉仪装置(200)提供激光信号,激光信号的频率同时锁定到所述法布里珀罗腔(102)和飞秒光梳装置(103),与此同时,所述飞秒光梳装置(103)将自身重复频率和零偏频率锁定到所述原子频标装置(104),使得所述激光装置最终输出激光信号频率同时兼具法布里珀罗腔的短期稳定性和原子频标的长期稳定性;The laser device (101) provides laser signals to the Fabry-Perot cavity device (102), the femtosecond optical comb device (103) and the ring cavity interferometer device (200) respectively, and the frequency of the laser signals is simultaneously locked to the the Fabry-Perot cavity (102) and the femtosecond optical comb device (103), at the same time, the femtosecond optical comb device (103) locks the self-repetition frequency and the zero-offset frequency to the atomic frequency scale a device (104), so that the final output laser signal frequency of the laser device has both the short-term stability of the Fabry-Perot cavity and the long-term stability of the atomic frequency scale; 所述高Q值环形腔干涉仪装置(200)用来构建被动式激光陀螺仪干涉光路,所述激光装置经过频率长期与短期的稳定之后输出激光信号分两路,分别沿逆时针方向和顺时针方向注入所述环形腔装置;沿逆时针方向注入激光信号作为长度基准,通过所述腔长频率锁定装置将所述环形腔装置谐振频率锁定到激光信号频率上,沿顺时针方向注入激光信号注入所述环形腔装置并将激光信号频率锁定至所述环形腔装置谐振频率上;The high-Q-value ring cavity interferometer device (200) is used to construct a passive laser gyroscope interference optical path, and the laser device outputs a laser signal in two paths after long-term and short-term frequency stabilization, which are respectively in a counterclockwise direction and a clockwise direction Inject the ring cavity device; inject the laser signal in the counterclockwise direction as the length reference, lock the resonant frequency of the ring cavity device to the frequency of the laser signal by the cavity length frequency locking device, and inject the laser signal in the clockwise direction. the ring cavity device and lock the frequency of the laser signal to the resonant frequency of the ring cavity device; 所述拍频探测装置(300)用于探测在所述高Q值环形腔干涉仪装置(200)之内分别沿逆时针方向和顺时针方向传播的激光信号频率之差Sagnac信号,以此来确定整个装置的旋转角速度。The beat frequency detection device (300) is used for detecting the Sagnac signal of the difference between the frequencies of the laser signals propagating in the counterclockwise direction and the clockwise direction respectively in the high-Q ring cavity interferometer device (200), so as to determine Rotational angular velocity of the entire device. 2.如权利要求1所述的被动式激光陀螺仪,其特征在于,所述被动式激光陀螺仪还包括:第一激光传输单元(105)、第一反馈单元(106)、第二激光传输单元(107)和第二反馈单元(108);2. The passive laser gyroscope according to claim 1, wherein the passive laser gyroscope further comprises: a first laser transmission unit (105), a first feedback unit (106), a second laser transmission unit ( 107) and a second feedback unit (108); 第二激光传输单元(107)的第一输入端连接至飞秒光梳装置(103)的输出端,第二激光传输单元(107)的第二输入端连接至激光装置(101)的输出端,第二反馈单元(108)的输入端连接至第二激光传输单元(107)的输出端,第二反馈单元(108)的输出端连接至(101)的第一输入端;The first input end of the second laser transmission unit (107) is connected to the output end of the femtosecond optical comb device (103), and the second input end of the second laser transmission unit (107) is connected to the output end of the laser device (101) , the input end of the second feedback unit (108) is connected to the output end of the second laser transmission unit (107), and the output end of the second feedback unit (108) is connected to the first input end of (101); 第一激光传输单元(105)的输入端连接至激光装置(101)的输出端,第一激光传输单元(105)的输入输出端与(102)连接,第一反馈单元(106)的输入端连接至第一激光传输单元(105)的输出端,第一反馈单元(106)的输出端连接至(101)的第二输入端;The input end of the first laser transmission unit (105) is connected to the output end of the laser device (101), the input and output end of the first laser transmission unit (105) is connected to (102), and the input end of the first feedback unit (106) is connected to the output end of the first laser transmission unit (105), and the output end of the first feedback unit (106) is connected to the second input end of (101); 第一激光传输单元(105)用于将激光装置(101)输出的激光信号传输至所述法布里珀罗腔(102);The first laser transmission unit (105) is configured to transmit the laser signal output by the laser device (101) to the Fabry-Perot cavity (102); 第一反馈单元(106)用于将激光装置(101)输出的激光信号频率锁定至所述法布里珀罗腔(102);The first feedback unit (106) is used to frequency-lock the laser signal output by the laser device (101) to the Fabry-Perot cavity (102); 第二激光传输单元(107)用于将激光装置(101)输出的激光信号传输至所述飞秒光梳装置(103);The second laser transmission unit (107) is configured to transmit the laser signal output by the laser device (101) to the femtosecond optical comb device (103); 第二反馈单元(108)用于将激光装置(101)输出的激光信号频率锁定至所述飞秒光梳装置(103)。The second feedback unit (108) is used for frequency locking the laser signal output by the laser device (101) to the femtosecond optical comb device (103). 3.如权利要求1所述的被动式激光陀螺仪,其特征在于,所述激光装置(101)输出的激光信号的频率由法布里珀罗腔装置(102)和链接到原子频标(104)的飞秒光梳装置(103)稳定。3. The passive laser gyroscope according to claim 1, wherein the frequency of the laser signal output by the laser device (101) is determined by the Fabry-Perot cavity device (102) and linked to the atomic frequency standard (104) ) of the femtosecond optical comb device (103) is stabilized. 4.如权利要求3所述的被动式激光陀螺仪,其特征在于,所述激光装置(101)输出的激光信号的频率短期稳定性由法布里珀罗腔(102)稳定,激光信号经第二分光镜(1051)所反射的一束激光通过第一电光调制器(1052)相位调制,后被光隔离器(1053)反射进法珀腔(102),该激光信号与法珀腔(102)相互作用后被反射,在第一光电探测器(1061)处探测信号,所得误差信号解调后经过第一伺服放大器(1062)后反馈给激光装置(101),将激光装置(101)输出激光信号频率锁定到法珀腔(102)谐振峰上,获得法珀腔(102)的优越短期稳定性;4. The passive laser gyroscope according to claim 3, wherein the short-term stability of the frequency of the laser signal output by the laser device (101) is stabilized by a Fabry-Perot cavity (102), and the laser signal is A laser beam reflected by the dichroic mirror (1051) is phase-modulated by the first electro-optic modulator (1052), and then reflected by the optical isolator (1053) into the Far-Pert cavity (102). ) are reflected after interacting, and the signal is detected at the first photodetector (1061), the obtained error signal is demodulated and fed back to the laser device (101) through the first servo amplifier (1062), and the laser device (101) outputs The frequency of the laser signal is locked to the resonance peak of the Fa-Per cavity (102), and the superior short-term stability of the Fa-Per cavity (102) is obtained; 所述激光装置(101)输出的激光信号的频率长期稳定性由链接到原子频标(104)的飞秒光梳(103)稳定,激光信号经第一分光镜(1012)所反射的一束激光与链接到原子频标装置(104)上的飞秒光梳装置(103)的出射激光信号经过第三分光镜(1071)后合成一束激光,在第二光电探测器(1081)上探测拍频信号,所得信号经过第二伺服放大器(1082)后反馈给激光装置(101),将激光装置输出激光信号频率锁定到链接到原子频标装置(104)的飞秒光梳装置(103)上,使得激光装置(101)具有了原子频标(104)的长期稳定性。The long-term stability of the frequency of the laser signal output by the laser device (101) is stabilized by a femtosecond optical comb (103) linked to the atomic frequency standard (104), and the laser signal is a beam reflected by the first beam splitter (1012). The laser beam and the outgoing laser signal of the femtosecond optical comb device (103) linked to the atomic frequency standard device (104) pass through the third beam splitter (1071) to synthesize a beam of laser light, which is detected on the second photodetector (1081) Beat frequency signal, the obtained signal is fed back to the laser device (101) after passing through the second servo amplifier (1082), and the frequency of the output laser signal of the laser device is locked to the femtosecond optical comb device (103) linked to the atomic frequency standard device (104) Therefore, the laser device (101) has the long-term stability of the atomic frequency standard (104). 5.如权利要求1所述的被动式激光陀螺仪,其特征在于,所述高Q值环形腔干涉仪装置(200)包括:陀螺激光准备单元(201)、第三激光传输单元(202)、第四激光传输单元(203)、环形腔(204)、第三反馈单元(205)和第四反馈单元(206);5. The passive laser gyroscope according to claim 1, wherein the high-Q ring cavity interferometer device (200) comprises: a gyro laser preparation unit (201), a third laser transmission unit (202), a fourth laser transmission unit (203), a ring cavity (204), a third feedback unit (205) and a fourth feedback unit (206); 第一激光信号接陀螺激光准备单元(201)的输入端,陀螺激光准备单元(201)的第一输出端连接至第三激光传输单元(202)的输入端,陀螺激光准备单元(201)的第二输出端连接至第四激光传输单元(203)的输入端,第三激光传输单元(202)的输入输出端与环形腔(204)连接,第四激光传输单元(203)的输入输出端与环形腔(204)连接;第三反馈单元(205)的输入端连接至第四激光传输单元(203)的第二输出端,第四反馈单元(206)的输入端连接至第三激光传输单元(202)的第二输出端;第三反馈单元(205)的输出端连接至环形腔(204)的另一输入端,第四反馈单元(206)的输出端连接至第四激光传输单元(203)的另一输入端;The first laser signal is connected to the input end of the gyro laser preparation unit (201), the first output end of the gyro laser preparation unit (201) is connected to the input end of the third laser transmission unit (202), and the The second output terminal is connected to the input terminal of the fourth laser transmission unit (203), the input and output terminals of the third laser transmission unit (202) are connected to the ring cavity (204), and the input and output terminals of the fourth laser transmission unit (203) connected to the ring cavity (204); the input end of the third feedback unit (205) is connected to the second output end of the fourth laser transmission unit (203), and the input end of the fourth feedback unit (206) is connected to the third laser transmission unit The second output end of the unit (202); the output end of the third feedback unit (205) is connected to the other input end of the ring cavity (204), and the output end of the fourth feedback unit (206) is connected to the fourth laser transmission unit The other input terminal of (203); 陀螺激光准备单元(201)用于将第一激光信号进行相位调制并等分成两束;A gyro laser preparation unit (201) is used to perform phase modulation on the first laser signal and equally divide it into two beams; 第三激光传输单元(202)用于将陀螺激光准备单元(201)输出的激光信号传输并注入至所述环形腔(204);The third laser transmission unit (202) is configured to transmit and inject the laser signal output by the gyro laser preparation unit (201) into the ring cavity (204); 第四激光传输单元(203)用于将陀螺激光准备单元(201)输出的另一激光信号传输并注入至所述环形腔(204);The fourth laser transmission unit (203) is used for transmitting and injecting another laser signal output from the gyro laser preparation unit (201) into the ring cavity (204); 环形腔(204)用于两束注入激光信号各自产生谐振并干涉;The ring cavity (204) is used for the two injected laser signals to resonate and interfere respectively; 第三反馈单元(205)用于将环形腔(204)谐振峰与沿逆时针方向注入的激光信号之间的误差信号伺服反馈至压电陶瓷(2045);The third feedback unit (205) is used for servo feedback of the error signal between the resonance peak of the ring cavity (204) and the laser signal injected in the counterclockwise direction to the piezoelectric ceramic (2045); 第四反馈单元(206)用于将环形腔(204)谐振峰与沿顺时针方向注入的激光信号之间的误差信号伺服反馈至第二声光调制器(2031)。The fourth feedback unit (206) is used for servo feedback of the error signal between the resonance peak of the ring cavity (204) and the laser signal injected in the clockwise direction to the second acousto-optic modulator (2031). 6.如权利要求5所述的被动式激光陀螺仪,其特征在于,所述环形腔(204)的腔长由沿逆时针方向注入的超稳激光稳定:6. The passive laser gyroscope according to claim 5, wherein the cavity length of the annular cavity (204) is stabilized by the ultra-stable laser injected in the counterclockwise direction: 沿逆时针方向注入第一激光信号经过第二电光调制器(2011)进行相位调制,相位调制后产生激光的载波信号和两个振幅相等、幅度相反的边带信号,边带直接被环形腔反射,载波与腔相互作用后与边带一起由所述第二法拉第隔离器(2033)反射到第三光电探测器(2051),由第三光电探测器(2051)探测激光载波频率与环形腔谐振峰的失谐量,解调得到误差信号,最终反馈到压电陶瓷(2045),来推动第四高反射率腔镜(2044),改变环形腔的腔长,将环形腔(204)的腔长锁定到沿逆时针注入激光信号的频率上。The first laser signal is injected in the counterclockwise direction, and the second electro-optic modulator (2011) is used for phase modulation. After phase modulation, the laser carrier signal and two sideband signals with equal and opposite amplitudes are generated. The sidebands are directly reflected by the ring cavity. , the carrier interacts with the cavity and is reflected by the second Faraday isolator (2033) together with the sideband to the third photodetector (2051), and the third photodetector (2051) detects the laser carrier frequency and the ring cavity resonance The detuning amount of the peak is obtained by demodulation, and the error signal is finally fed back to the piezoelectric ceramic (2045) to drive the fourth high reflectivity cavity mirror (2044), change the cavity length of the annular cavity, and connect the cavity of the annular cavity (204) long lock to the frequency of the laser signal injected counterclockwise. 7.如权利要求5或6所述的被动式激光陀螺仪,其特征在于,沿顺时针方向注入的超稳激光信号通过第二声光调制器(2031),频率锁定到所述环形腔(204)的腔长上,其中:7. The passive laser gyroscope according to claim 5 or 6, characterized in that, the ultra-stable laser signal injected in the clockwise direction passes through the second acousto-optic modulator (2031), and the frequency is locked to the ring cavity (204) ) on the cavity length, where: 沿顺时针方向注入激光信号边带被环形腔反射,载波与腔相互作用后与边带一起由所述第一法拉第隔离器(2023)反射到第四光电探测器(2061),由第四光电探测器(2061)探测激光载波频率与环形腔谐振峰的失谐量,解调得到误差信号,最终反馈到第二声光调制器驱动压控振荡器(2063),来改变第二声光调制器的调制频率f2,使得沿顺时针方向注入激光的频率与环形腔谐振,将沿顺时针方向注入激光的频率锁定到环形腔腔长上。The sideband of the laser signal injected in the clockwise direction is reflected by the annular cavity, and after the carrier interacts with the cavity, it is reflected by the first Faraday isolator (2023) together with the sideband to the fourth photodetector (2061), and the fourth photoelectric The detector (2061) detects the detuning amount between the laser carrier frequency and the resonant peak of the ring cavity, demodulates the error signal, and finally feeds it back to the second acousto-optic modulator to drive the voltage-controlled oscillator (2063) to change the second acousto-optic modulation The modulation frequency f 2 of the device is adjusted so that the frequency of the laser injected in the clockwise direction resonates with the ring cavity, and the frequency of the laser injected in the clockwise direction is locked to the length of the ring cavity. 8.如权利要求1所述的被动式激光陀螺仪,其特征在于,Sagnac信号既可以利用第一声光调制器(2021)和第二声光调制器(2031)的调制频率之差得到,也可以利用从腔后两个方向的溢出光拍频探测得到。8. The passive laser gyroscope of claim 1, wherein the Sagnac signal can be obtained by using the difference between the modulation frequencies of the first acousto-optic modulator (2021) and the second acousto-optic modulator (2031), or It can be detected by the beat frequencies of spillover light from two directions behind the cavity.
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CN110243511A (en) * 2019-06-28 2019-09-17 暨南大学 A high-sensitivity optical fiber Fabry-Perot stress sensor and its sensing method
CN110702090A (en) * 2019-10-29 2020-01-17 西安电子科技大学 High-precision lock-zone-free laser gyro device and method
CN110702090B (en) * 2019-10-29 2022-05-03 西安电子科技大学 High-precision lock-zone-free laser gyro device and method
CN111413859B (en) * 2020-04-27 2021-07-02 深港产学研基地(北京大学香港科技大学深圳研修院) Iodine molecule optical clock based on pulse modulation wide-spectrum comb-tooth laser and control method thereof
CN111413859A (en) * 2020-04-27 2020-07-14 深港产学研基地(北京大学香港科技大学深圳研修院) Iodine molecule optical clock based on pulse modulation wide-spectrum comb-tooth laser and control method thereof
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CN112180394A (en) * 2020-09-02 2021-01-05 浙江大学 Multi-longitudinal-mode high-spectral-resolution laser radar interferometer frequency locking system
CN112180394B (en) * 2020-09-02 2023-11-03 浙江大学 A multi-longitudinal mode high spectral resolution laser radar interferometer frequency locking system
CN112857355A (en) * 2021-01-08 2021-05-28 华中科技大学 Passive laser gyroscope based on polarization selection locking and angular velocity determination method
CN112857355B (en) * 2021-01-08 2022-09-20 华中科技大学 Passive laser gyroscope and angular velocity determination method based on polarization selective locking
CN113916211A (en) * 2021-09-13 2022-01-11 华中科技大学 A Passive Laser Gyroscope Based on Critically Coupled Ring Cavity
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