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CN104155642A - Traceable synchronous measurement ruler-based mixed double-light source laser range finding device and method - Google Patents

Traceable synchronous measurement ruler-based mixed double-light source laser range finding device and method
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CN104155642A
CN104155642ACN201410263593.0ACN201410263593ACN104155642ACN 104155642 ACN104155642 ACN 104155642ACN 201410263593 ACN201410263593 ACN 201410263593ACN 104155642 ACN104155642 ACN 104155642A
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laser
frequency
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input end
beam splitter
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CN104155642B (en
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谭久彬
杨宏兴
胡鹏程
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Harbin Institute of Technology Shenzhen
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Harbin Institute of Technology Shenzhen
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Abstract

Translated fromChinese

基于可溯源同步测尺的混合双光源激光测距装置与方法属于相位激光测距技术,所述测距装置包括测尺生成单元、激光移频单元、扩束准直镜组、测量光路及电路单元;其测距方法包括步骤如下:步骤一、开启频率基准激光器和双纵模稳频He-Ne激光器与半导体激光器;步骤二、一束作为参考激光束,另一束作为测量激光;步骤三、以作为精测尺;步骤四、以作为粗测尺;步骤五、移动测量角椎棱镜至目标端,分别得到精测尺与粗测尺的相位差φ1和φ2,最后通过公式得到被测距离值;本发明解决了相位激光测距技术中缺少一种能兼顾大功率、多测尺同步性与可溯源性的激光测距装置与方法的问题,具有测距精度高、测量效率高、稳定性和实时性强的特点。

The hybrid dual light source laser ranging device and method based on a traceable synchronous measuring ruler belongs to the phase laser ranging technology, and the ranging device includes a measuring ruler generating unit, a laser frequency shifting unit, a beam expanding collimating lens group, a measuring optical path and a circuit unit; its ranging method includes steps as follows: Step 1, open frequency reference laser and dual longitudinal mode frequency stabilized He-Ne laser and semiconductor laser; Step 2, one beam as reference laser beam, another beam as measuring laser; Step 3 ,by As a precise measuring ruler; step 4, take As a coarse measuring ruler; Step 5, move the measuring corner cone prism to the target end, obtain the phase difference φ1 and φ2 of the fine measuring ruler and the coarse measuring ruler respectively, and finally obtain the measured distance value through the formula; the present invention solves the problem of phase laser The lack of a laser ranging device and method that can take into account high power, multi-scale synchronization and traceability in ranging technology has the characteristics of high ranging accuracy, high measurement efficiency, stability and real-time performance.

Description

The two light source laser ranging systems of mixing and method based on the same pacing chi of can tracing to the source
Technical field
The invention belongs to phase place laser measuring technique, relate generally to a kind of phase laser distance apparatus and method.
Background technology
Large-scale metrology receives much concern in the large-scale optical, mechanical and electronic integration equipment processing and manufacturings such as the machine-building of development large-scale precision, great scientific and technological engineering, aerospace industry, shipping industry and microelectronics equipment industry, wherein several meters of large-scale metrologies to hundreds of rice scope are large parts processing and the whole important foundations of assembling in aerospace vehicle and jumbo ship, the quality of its measuring method and equipment performance directly affects workpiece quality and assembly precision, and then running quality, performance and the life-span of a whole set of equipment of impact.The chi phase ranging methods of surveying utilize one group of survey chi wavelength from big to small to the measurement of refining step by step of tested distance more, solve conflicting between measurement range and measuring accuracy, can in hundreds of meters of overlength operating distances, reach submillimeter to micron-sized static measurement precision.
, survey in chi phase laser distance technology more, although the mode that many survey chis are measured has step by step been taken into account the demand of measurement range and measuring accuracy, but the restriction due to light source technology, bigness scale chi and accurate measurement chi can not produce the line phase of going forward side by side simultaneously and measure, caused Measuring Time long, the problem that measurement result real-time is poor, on the other hand due to take in surveying chi phase laser distance technology survey chi wavelength size and measure as benchmark, the stability of surveying chi wavelength directly affects the precision of laser ranging, therefore how to obtain bigness scale chi and the accurate measurement chi wavelength of high stability, and make it to participate in measuring is to improve at present the subject matter of surveying chi phase laser distance precision and real-time more simultaneously.
The stability of surveying chi is relevant with light source technology with synchronous generating technique, and by known to the analysis of phase laser distance method LASER Light Source technology, the modulation means of phasic difference method has directly modulation of electric current, optical modulation and intermode beat frequency modulation system etc. both at home and abroad at present.
Direct current modulation method is utilized semiconductor laser, and the feature of light intensity curent change comes the output intensity of noise spectra of semiconductor lasers to modulate, and has the advantages such as the modulation of being simple and easy to.Document [Siyuan Liu, Jiubin Tan and Binke Hou. Multicycle Synchronous Digital Phase Measurement Used to Further Improve Phase-Shift Laser Range Finding. Meas. Sci. Technol. 2007, 18:1756 – 1762] and patent [the large range high precision fast laser ranging apparatus and method of multiple frequency synchronous modulation, publication number: CN1825138] all set forth a kind of current modulating method of based semiconductor laser instrument, it adopts the synthetic composite signal of multiple frequency synchronous to carry out synchronous modulation to laser output power, realized at synchronization and obtained in multifrequency modulation range finding each modulation frequency for the measurement result of tested distance, but in order to obtain linear modulation, make the straight line portion of working point in output characteristic curve, must when adding modulation signal electric current, add a suitable bias current makes its output signal undistorted, the introducing of direct current biasing has strengthened power consumption, when working long hours, temperature raises, can affect the stability of Output optical power, cause modulation waveform distortion, and the increase along with modulating frequency, depth of modulation can reduce, cause modulation waveform distortion, can not carry out high frequency modulated, size and the degree of stability of accurate measurement chi wavelength have been limited, on the other hand in the actual application of large-scale metrology, laser easily causes the loss of laser power in long Distance Transmission process, cause the impact on modulation waveform, and then accuracy and the degree of stability of impact survey chi, its frequency stability of surveying chi is generally less than 10-7.
Utilize light modulating method to be mainly acoustooptic modulation method and electro-optic modulation method, its modulation band-width is subject to the multifactorial impact of laser beam diameter etc., also can bring waveform distortion, particularly just even more serious when high frequency (Gigahertz), therefore it forms large survey chi, and measuring accuracy is difficult to improve owing to being subject to the restriction of maximum modulation frequency.
Utilize laser instrument different mode to export formed beat signal as the method for surveying chi, be called intermode modulation.The chamber long correlation of the modulation band-width of the method and laser instrument, He-Ne laser frequency stabilization technology is ripe, its frequency stability is high, the degree of stability of the survey chi being obtained by it is high, patent [high precision multiple frequency synchronous phase laser distance apparatus and method, publication number: CN 102419166] and patent [the multiple frequency synchronous phase laser distance apparatus and method based on dual-acousto-optic shift, publication number: CN 102305591A] all utilized the intermode modulation of He-Ne laser instrument and in conjunction with acousto-optic frequency translation technology, high-precision accurate measurement chi and bigness scale chi have been obtained, but the survey chi that the method produces does not possess tractability, when it is measured, absolute measuring chi length needs another detection system to provide, increased the complicacy of measuring, on the other hand, this method of utilizing process of heterodyning to obtain accurate measurement chi phase place, the frequency of its processing signals is higher, can follow-up phase measurement difficulty and measuring accuracy be affected, and supposes that phase-measurement accuracy is 0.05o, range measurement accuracy will reach 1um-10um, and signal frequency is at least 2GHz-20GHz, far exceeds the bandwidth of signal processing circuit.
Patent [superheterodyne device and method of reseptance and receiving trap SIC (semiconductor integrated circuit), publication number: CN102484492A] all introduced a kind of superhet interference signal treatment technology, Zhang Cunman [the Zhang Cunman etc. of Tsing-Hua University, superhet is interfered absolute distance measurement Review Study, optical technology 1998, (1): 7-9.] introduced superhet absolute distance measurement method, the method has reduced the processing frequency of signal, more easily reaches higher measuring accuracy.But this technology is on the one hand, can only obtain one and survey chi, and not possess tractability, can not carry out the chis of surveying more and measure, let alone survey the synchronism of chi more; To obtain surveying chi wavelength less for superhet on the other hand, generally in micron dimension, and can only be for the measurement of the micro-shape in surface.
In order to improve the stability of laser instrument output frequency, occurred usining that the Output of laser frequency of iodine saturated absorption frequency stabilization laser instrument, as the frequency-stabilizing method of frequency stabilization benchmark, utilizes the saturated absorption spectra of iodine to carry out rrequency-offset-lock control to He-Ne laser instrument and semiconductor laser.China is also studied, such as patent ZL200910072518.5 and patent ZL200910072519.X etc., a kind of rrequency-offset-lock device that utilizes iodine saturated absorption He-Ne frequency stabilized laser has all been described, make the laser output frequency after rrequency-offset-lock there is very high frequency stability, have advantages of that output frequency can trace to the source, but the output frequency of laser reaches 1014hz, corresponding survey chi is between 400-700nm, and measurement range, in nm rank, can not be found range for long distance laser, needs badly a kind ofly high frequency stability laser frequency is converted to the laser ranging on a large scale that can trace to the source surveys chi, and synchronizes them the technology of generation.
In sum, in phase laser distance technology, lack a kind of can taking into account at present and survey the synchronisms of chi and the precision distance measurement apparatus and method of tractability more.
Summary of the invention
The object of the invention is in existing phase laser distance technology, to lack a kind of problems that can take into account many survey synchronisms of chi and the apparatus and method of traceability in order to solve, a kind of mixing based on the same pacing chi of can tracing to the source pair light source laser ranging systems and method are provided, reach the object of increase range finding dirigibility, simplification range finding step, raising measurement efficiency and precision and degree of stability, real-time.
The two light source laser ranging systems of a kind of mixing based on the same pacing chi of can tracing to the source, by surveying chi generation unit, laser shift frequency unit, beam-expanding collimation mirror group and optical path and circuit unit, form, the Laser output that survey chi generation unit sends is to the input end of laser shift frequency unit, output Yi road, laser shift frequency unit laser outputs to an input end of optical path and circuit unit by beam-expanding collimation mirror group, another road laser of laser shift frequency unit output is directly inputted to another input end of optical path and circuit unit;
The structure of described survey chi generation unit is: the laser beam of frequency reference laser instrument transmitting arrives the input end of optical splitter, the first output terminal of optical splitter connects No. two spectroscopical input ends, No. two spectroscopical output terminals connect the input end of a photodetector, the second output terminal of optical splitter connects No. two spectroscopical input ends, No. two spectroscopical output terminals connect the input end of No. two photodetectors, No. one photodetector is connected the input end of single-chip microcomputer with the output terminal of No. two photodetectors, long two input ends adjusting actuator of two output terminal connection chambers of single-chip microcomputer, long two output terminals adjusting actuator in chamber connect respectively the input end of semiconductor laser and two longitudinal mode He-Ne laser instruments, an output terminal of semiconductor laser connects No. three spectroscopical input ends, No. three spectroscopical output terminals connect the input end of a catoptron, the output terminal of a catoptron connects the input end of a polaroid, an output terminal of two longitudinal mode He-Ne laser instruments connects No. two spectroscopical input ends,
The structure of described laser shift frequency unit is: an output terminal surveying chi generation unit connects the input end of No. nine catoptrons, the output terminal of No. nine catoptrons connects No. three spectroscopical input ends, No. three spectroscopical output terminal connects No. four spectroscopical input ends, another output terminal of surveying chi generation unit connects the input end of a polarization spectroscope, an output terminal of a polarization spectroscope connects the input end of a half-wave plate, the output terminal of a half-wave plate connects the input end of No. two polarization spectroscopes, an output terminal of No. two polarization spectroscopes connects an input end of No. three polarization spectroscopes, another output terminal of No. two polarization spectroscopes connects the input end of No. four catoptrons, the output terminal of No. four catoptrons connects an input end of a laser frequency shifter, the output terminal of a DDS signal source connects another input end of a laser frequency shifter, the output terminal of a laser frequency shifter connects the input end of No. five catoptrons, the output terminal of No. five catoptrons connects another input end of No. three polarization spectroscopes, the output terminal of No. three polarization spectroscopes connects No. three spectroscopical another input ends, No. three spectroscopical output terminal connects input end of No. four spectroscopes, another output terminal of a polarization spectroscope connects the input end of No. six catoptrons, the output terminal of No. six catoptrons is through the input end of No. four polarization spectroscopes of No. two half-wave plate connections, an output terminal of No. four polarization spectroscopes connects an input end of No. five polarization spectroscopes, another output terminal of No. four polarization spectroscopes connects the input end of No. seven catoptrons, the output terminal of No. seven catoptrons connects an input end of No. two laser frequency shifters, the output terminal of No. two DDS signal sources connects another input end of No. two laser frequency shifters, the output terminal of No. two laser frequency shifters connects the input end of No. eight catoptrons, the output terminal of No. eight catoptrons connects another input end of No. five polarization spectroscopes, the output terminal of No. five polarization spectroscopes connects No. four spectroscopical another input ends,
The structure of described optical path and circuit unit is: an output terminal of laser shift frequency unit connects the input end of ten No. two catoptrons, the output terminal of ten No. two catoptrons connects the input end of No. five catoptrons, an output terminal of No. five catoptrons is communicated with the input end of No. three photodetectors by No. two polaroids, the output terminal of No. three photodetectors connects the input end of a low-pass filter, the output terminal of a low-pass filter connects an input end of a frequency mixer, an output terminal of No. three DDS signal sources connects another input end of a frequency mixer, the output terminal of a frequency mixer connects an input end of a phase detector, another output terminal of No. five catoptrons is communicated with the input end of No. four photodetectors by No. three polaroids, the output terminal of No. four photodetectors connects the input end of No. two low-pass filters, the output terminal of No. two low-pass filters connects an input end of No. two phase detectors, the output terminal of beam-expanding collimation mirror group connects an input end of No. six polarization spectroscopes, an output terminal of No. six polarization spectroscopes is communicated with the input end of No. ten catoptrons by a quarter-wave plate, the output terminal of No. ten catoptrons is communicated with an input end of No. six polarization spectroscopes by a quarter-wave plate, an output terminal of No. six polarization spectroscopes is communicated with the input end of ride on Bus No. 11 catoptron by No. two quarter-wave plates, the output terminal of ride on Bus No. 11 catoptron is communicated with another input end of No. six polarization spectroscopes by No. two quarter-wave plates, another output terminal of No. six polarization spectroscopes connects No. eight spectroscopical input ends, No. eight a spectroscopical output terminal is communicated with the input end of No. five photodetectors by No. four polaroids, the output terminal of No. five photodetectors connects the input end of No. three low-pass filters, the output terminal of No. three low-pass filters connects an input end of No. three frequency mixer, another output terminal of No. three DDS signal sources connects another input end of No. three frequency mixer, the output terminal of No. three frequency mixer connects another input end of a phase detector, No. eight spectroscopical another output terminal is communicated with the input end of No. six photodetectors by No. five polaroids, the output terminal of No. six photodetectors connects the input end of No. four low-pass filters, the output terminal of No. four low-pass filters connects another input end of No. two phase detectors.
The two light source laser distance measurement methods of mixing based on the same pacing chi of can tracing to the source, its concrete steps are as follows:
Step 1, open frequency benchmark laser, semiconductor laser, two longitudinal mode He-Ne laser instrument, after through preheating and frequency stabilization, pass through FEEDBACK CONTROL, within semiconductor laser and two longitudinal mode He-Ne laser instrument output frequencies are locked in to the certain frequency scope of frequency reference laser instrument, semiconductor laser output frequency, through a polaroid, is adjusted polarization angle and is made only to allow frequency bev1laser pass through, two longitudinal mode He-Ne laser instrument output frequencies are v2and v3double-frequency laser;
Step 2, by the laser of the formed three kinds of frequencies of step 1, enter laser shift frequency unit, wherein a branch of double-frequency laser separates frequency with a polarization spectroscope and isv2withv3two bundle laser, separate two bundle double-frequency lasers with No. two polarization spectroscopes and No. four polarization spectroscopes respectively again through after half-wave plate, and wherein a road is through laser frequency shifter, and by DDS signal source driving laser frequency shifter, frequency is respectivelyf1withf2, the laser of last various frequencies merges, and wherein has five kinds of frequencies, is respectivelyv1,v2,v3,v2+f1withv3+f2,, this Shu Jiguang incides Amici prism and is divided into two-beam, and a branch of conduct is with reference to laser beam, and another Shu Zuowei measures laser beam and shines measurement target;
Step 3, reference laser beam are divided into two bundle laser beam through Amici prism, beam of laser bundle through polarization direction withv1after No. two identical polaroids, frequency isv1,v2withv3the polarization laser of horizontal direction enter into No. three photodetectors and change, its output electrical signals, its frequency isv1-v2,using this as bigness scale chi, another beam of laser through polarization direction withv1after becoming No. three polaroids of 45 degree, incide photodetector No. four, the electric signal of No. four photodetector outputs through low-pass filter filtering high frequency electrical signal, retain low frequency electric signal, its frequency isf1-f2, using this as accurate measurement chi;
When step 4, measurement start, No. ten catoptrons of reference surface maintain static, mobile ride on Bus No. 11 catoptron 53 is to destination end, measuring distance is L, measuring beam is after measuring catoptron reflection, and the light beam reflecting with reference surface converges at No. six polarization spectroscope places, enters metering circuit, measure laser beam and be divided into two bundle laser beam through Amici prism, wherein beam of laser bundle through polarization direction withv1after No. four identical polaroids, frequency isv1,v2withv3the polarization laser of horizontal direction enter into No. six photodetectors and change, its output electrical signals, its frequency isv1-v2,using this as bigness scale chi, and survey chi length is, another beam of laser through polarization direction withv1after becoming No. five polaroids of 45 degree, incide photodetector No. five, the electric signal of No. five photodetector outputs through low-pass filter filtering high frequency electrical signal, retain low frequency electric signal, its frequency isf1-f2, using this as accurate measurement chi, survey chi length is;
Step 5, by a phase detector and No. two phase detectors, obtain respectively frequency and bev1-v2withf1-f2the phase differential of two path signalφ1withφ2, according to formulatry to achieve the distance measure of bigness scale chilc, and its substitution formula is tried to achieve to the phase place round values of accurate measurement chi; Whereinfloor(x) function returnsxthe integral part of value, finally according to formula, try to achieve tested distance value:, in formula: c is the light velocity, the air refraction that n is environment.
Feature of the present invention and beneficial effect are:
The first, the present invention proposes, accurate measurement chi production method thick based on tracing to the source of mixing laser and device, these apparatus and method are utilized frequency reference type frequency reference laser instrument, and frequency stability reaches 10-11to 10-12magnitude, a semiconductor laser and a He-Ne laser instrument are carried out to rrequency-offset-lock control, and utilize semiconductor laser after frequency stabilization and He-Ne laser to form required thick of range finding, accurate measurement chi, make Output of laser frequency and formed laser ranging survey chi wavelength and can directly be traceable to frequency/wavelength benchmark, and can adjust according to actual needs lock point, and then regulate surveying chi wavelength, increased the dirigibility of range finding, overcome and in existing distance measuring equipment, surveyed the shortcoming that chi is not directly traced to the source, simplify general distance measuring equipment and when absolute measuring is long, surveyed the link that chi wavelength needs another detection system to detect, improved measurement efficiency and precision, this is that the present invention distinguishes one of innovative point of existing apparatus.
The second, the present invention proposes a kind of many surveys chi phase-locking acquisition methods and device of being combined with superhet based on heterodyne.These apparatus and method utilize laser frequency shifter to carry out shift frequency to the laser of component frequency, produce the laser of multi-frequency, and utilize heterodyne approach and superhet method to obtain respectively bigness scale chi and accurate measurement chi simultaneously, and then make it to participate in to measure simultaneously, realized the synchro measure of thick accurate measurement chi phase place, shorten Measuring Time, improved the real-time of measurement result.The laser interferometry combining with superhet by heterodyne obtains test phase signal, eliminate common mode interference, improved the degree of stability of surveying chi, reduced the frequency of phase measuring circuit reception signal simultaneously, reduce the difficulty of circuit design, this is two of the present invention's innovative point of distinguishing existing apparatus.
The 3rd, the present invention adopts He-Ne laser instrument and semiconductor laser to form thick accurate measurement chi generation hybrid light source, ensureing the complexity of having simplified light source under the prerequisite that survey chi can be traced to the source, and can make full use of semiconductor laser light resource and He-Ne laser instrument advantage separately, first utilize the large feature of semiconductor Output of laser energy, can guarantee light echo energy, improve signal to noise ratio (S/N ratio), next utilizes He-Ne laser instrument frequency stabilization process feature simply rapidly, can quick adjustment Output of laser frequency, and then regulate surveying chi, this is three of the present invention's innovative point of distinguishing existing apparatus.
Accompanying drawing explanation
Fig. 1 is the general structure schematic diagram of laser ranging system of the present invention;
Fig. 2 is for surveying the structural representation of chi generation unit;
Fig. 3 is the structural representation of laser shift frequency unit;
Fig. 4 is the structural representation of optical path and circuit unit.
Piece number explanation in figure: 1, survey chi generation unit, 2, laser shift frequency unit, 3, beam-expanding collimation mirror group, 4, optical path and circuit unit, 5, frequency reference laser instrument, 6, optical splitter, 7, a spectroscope, 8, No. two spectroscopes, 9, a photodetector, 10, No. two photodetectors, 11, single-chip microcomputer, 12, the long actuator of adjusting in chamber, 13, semiconductor laser, 14, two longitudinal mode He-Ne laser instruments, 15, No. three spectroscopes, 16, a catoptron, 17, a polaroid, 18, a polarization spectroscope, 19, a half-wave plate, 20, No. two polarization spectroscopes, 21, No. four catoptrons, 22, a DDS signal source, 23, a laser frequency shifter, 24, No. five catoptrons, 25, No. three polarization spectroscopes, 26, No. three spectroscopes, 27, No. six catoptrons, 28, a half-wave plate, 29, No. four polarization spectroscopes, 30, No. seven catoptrons, 31, No. two DDS signal sources, 32, No. two laser frequency shifters, 33, No. eight catoptrons, 34, No. five polarization spectroscopes, 35, No. nine catoptrons, 36, No. four spectroscopes, 37, ten No. two catoptrons, 38, No. five catoptrons, 39, No. two polaroids, 40, No. three photodetectors, 41, a low-pass filter, 42, a frequency mixer, 43, No. three DDS signal sources, 44, a phase detector, 45, No. three polaroids, 46, No. four photodetectors, 47, No. two low-pass filters, 48, No. two phase detectors, 49, No. six polarization spectroscopes, 50, a quarter-wave plate, 51, No. ten catoptrons, 52, No. two quarter-wave plates, 53, ride on Bus No. 11 catoptron, 54, No. eight spectroscopes, 55, No. four polaroids, 56, No. five photodetectors, 57, No. three low-pass filters, 58, No. three frequency mixer, 59, No. five polaroids, 60, No. six photodetectors, 61, No. four low-pass filters.
Embodiment
Below in conjunction with accompanying drawing, embodiment of the present invention is described in detail.
The two light source laser ranging systems of a kind of mixing based on the same pacing chi of can tracing to the source, comprise beam-expanding collimation mirror group 3, described device is by surveying chi generation unit 1, laser shift frequency unit 2, beam-expanding collimation mirror group 3 and optical path and circuit unit 4 form, the Laser output that survey chi generation unit 1 sends is to the input end of laser shift frequency unit 2, laser shift frequency unit 2 output Yi road laser output to an input end of optical path and circuit unit 4 by beam-expanding collimation mirror group 3, another road laser of laser shift frequency unit 2 outputs is directly inputted to another input end of optical path and circuit unit 4,
The structure of described survey chi generation unit 1 is: the laser beam of frequency reference laser instrument 5 transmittings arrives the input end of optical splitter 6, the first output terminal of optical splitter 6 connects an input end of No. two spectroscopes 7, an output terminal of No. two spectroscopes 7 connects the input end of a photodetector 9, the second output terminal of optical splitter 6 connects an input end of No. two spectroscopes 8, the output terminal of No. two spectroscopes 8 connects the input end of No. two photodetectors 10, No. one photodetector 9 is connected the input end of single-chip microcomputer 11 with the output terminal of No. two photodetectors 10, long two input ends adjusting actuator 12 of two output terminal connection chambers of single-chip microcomputer 11, long two output terminals adjusting actuator 12 in chamber connect respectively the input end of semiconductor laser 13 and two longitudinal mode He-Ne laser instruments 14, an output terminal of semiconductor laser 13 connects an input end of No. three spectroscopes 15, an output terminal of No. three spectroscopes 15 connects the input end of a catoptron 16, the output terminal of a catoptron 16 connects the input end of a polaroid 17, an output terminal of two longitudinal mode He-Ne laser instruments 14 connects an input end of No. two spectroscopes 8,
The structure of described laser shift frequency unit 2 is: an output terminal surveying chi generation unit 1 connects the input end of No. nine catoptrons 35, the output terminal of No. nine catoptrons 35 connects an input end of No. three spectroscopes 26, the output terminal of No. three spectroscopes 26 connects an input end of No. four spectroscopes 36, another output terminal of surveying chi generation unit 1 connects the input end of a polarization spectroscope 18, an output terminal of a polarization spectroscope 18 connects the input end of a half-wave plate 19, the output terminal of a half-wave plate 19 connects the input end of No. two polarization spectroscopes 20, an output terminal of No. two polarization spectroscopes 20 connects an input end of No. three polarization spectroscopes 25, another output terminal of No. two polarization spectroscopes 20 connects the input end of No. four catoptrons 21, the output terminal of No. four catoptrons 21 connects an input end of a laser frequency shifter 23, the output terminal of a DDS signal source 22 connects another input end of a laser frequency shifter 23, the output terminal of a laser frequency shifter 23 connects the input end of No. five catoptrons 24, the output terminal of No. five catoptrons 24 connects another input end of No. three polarization spectroscopes 25, the output terminal of No. three polarization spectroscopes 26 connects another input end of No. three spectroscopes 26, the output terminal of No. three spectroscopes 26 connects 36 1 input ends of No. four spectroscopes, another output terminal of a polarization spectroscope 18 connects the input end of No. six catoptrons 27, the output terminal of No. six catoptrons 27 is through the input end of No. four polarization spectroscopes 29 of No. two half-wave plate 28 connections, an output terminal of No. four polarization spectroscopes 29 connects an input end of No. five polarization spectroscopes 34, another output terminal of No. four polarization spectroscopes 29 connects the input end of No. seven catoptrons 30, the output terminal of No. seven catoptrons 30 connects an input end of No. two laser frequency shifters 32, the output terminal of No. two DDS signal sources 31 connects another input end of No. two laser frequency shifters 32, the output terminal of No. two laser frequency shifters 32 connects the input end of No. eight catoptrons 33, the output terminal of No. eight catoptrons 33 connects another input end of No. five polarization spectroscopes 34, the output terminal of No. five polarization spectroscopes 34 connects another input end of No. four spectroscopes 36,
The structure of described optical path and circuit unit 4 is: an output terminal of laser shift frequency unit 2 connects the input end of ten No. two catoptrons 37, the output terminal of ten No. two catoptrons 37 connects the input end of No. five catoptrons 38, an output terminal of No. five catoptrons 38 is communicated with the input end of No. three photodetectors 40 by No. two polaroids 39, the output terminal of No. three photodetectors 40 connects the input end of a low-pass filter 41, the output terminal of a low-pass filter 41 connects an input end of a frequency mixer 42, an output terminal of No. three DDS signal sources 43 connects another input end of a frequency mixer 42, the output terminal of a frequency mixer 42 connects an input end of a phase detector 44, another output terminal of No. five catoptrons 38 is communicated with the input end of No. four photodetectors 46 by No. three polaroids 45, the output terminal of No. four photodetectors 46 connects the input end of No. two low-pass filters 47, the output terminal of No. two low-pass filters 47 connects an input end of No. two phase detectors 48, the output terminal of beam-expanding collimation mirror group 3 connects an input end of No. six polarization spectroscopes 49, an output terminal of No. six polarization spectroscopes 49 is communicated with the input end of No. ten catoptrons 51 by a quarter-wave plate 50, the output terminal of No. ten catoptrons 51 is communicated with an input end of No. six polarization spectroscopes 49 by a quarter-wave plate 50, an output terminal of No. six polarization spectroscopes 49 is communicated with the input end of ride on Bus No. 11 catoptron 53 by No. two quarter-wave plates 52, the output terminal of ride on Bus No. 11 catoptron 53 is communicated with another input end of No. six polarization spectroscopes 49 by No. two quarter-wave plates 52, another output terminal of No. six polarization spectroscopes 49 connects an input end of No. eight spectroscopes 54, an output terminal of No. eight spectroscopes 54 is communicated with the input end of No. five photodetectors 56 by No. four polaroids 55, the output terminal of No. five photodetectors 56 connects the input end of No. three low-pass filters 57, the output terminal of No. three low-pass filters 57 connects an input end of No. three frequency mixer 58, another output terminal of No. three DDS signal sources 43 connects another input end of No. three frequency mixer 58, the output terminal of No. three frequency mixer 58 connects another input end of a phase detector 44, another output terminal of No. eight spectroscopes 54 is communicated with the input end of No. six photodetectors 60 by No. five polaroids 59, the output terminal of No. six photodetectors 60 connects the input end of No. four low-pass filters 61, the output terminal of No. four low-pass filters 61 connects another input end of No. two phase detectors 48.
One, No. two laser frequency shifter 23,32 of described laser shift frequency unit 2 comprises acousto-optic frequency shifters, electro-optic frequency translation device, and laser frequency can regulate.
Described survey chi generation unit 1 medium frequency benchmark laser 5 comprises iodine stabilized laser, femtosecond laser frequency comb laser instrument, and frequency stability is better than 10-12.
The two light source laser distance measurement methods of mixing based on the same pacing chi of can tracing to the source, its concrete steps are as follows:
Step 1, open frequency benchmark laser 5, semiconductor laser 13, two longitudinal mode He-Ne laser instrument 14, after through preheating and frequency stabilization, pass through FEEDBACK CONTROL, within semiconductor laser 13 and two longitudinal mode He-Ne laser instrument 14 output frequencies are locked in to the certain frequency scope of frequency reference laser instrument 5, semiconductor laser 13 output frequencies, through a polaroid 17, are adjusted polarization angle and are made only to allow frequency bev1laser pass through, two longitudinal mode He-Ne laser instrument 14 output frequencies are v2and v3double-frequency laser;
Step 2, by the laser of the formed three kinds of frequencies of step 1, enter laser shift frequency unit 2, wherein a branch of double-frequency laser separates frequency with a polarization spectroscope 18 and isv2withv3two bundle laser, separate two bundle double-frequency lasers with No. two polarization spectroscopes 20 and No. four polarization spectroscopes 29 respectively again through after half-wave plate, and wherein a road is through laser frequency shifter, and by DDS signal source driving laser frequency shifter, frequency is respectivelyf1withf2, the laser of last various frequencies merges, and wherein has five kinds of frequencies, is respectivelyv1,v2,v3,v2+f1withv3+f2,, this Shu Jiguang incides Amici prism and is divided into two-beam, and a branch of conduct is with reference to laser beam, and another Shu Zuowei measures laser beam and shines measurement target;
Step 3, reference laser beam are divided into two bundle laser beam through Amici prism, beam of laser bundle through polarization direction withv1after No. two identical polaroids 39, frequency isv1,v2withv3the polarization laser of horizontal direction enter into No. three photodetectors 40 and change, its output electrical signals, its frequency isv1-v2,using this as bigness scale chi, another beam of laser through polarization direction withv1the electric signal that becomes to incide after No. three polaroids 45 of 45 degree 46 outputs of 46, No. four photodetectors of No. four photodetectors through low-pass filter filtering high frequency electrical signal, retain low frequency electric signal, its frequency isf1-f2, using this as accurate measurement chi;
When step 4, measurement start, No. ten catoptrons 51 of reference surface maintain static, mobile ride on Bus No. 11 catoptron 53 is to destination end, measuring distance is L, measuring beam is after measuring catoptron 53 reflections, and the light beam reflecting with reference surface converges at No. six polarization spectroscope 49 places, enters metering circuit, measure laser beam and be divided into two bundle laser beam through Amici prism, wherein beam of laser bundle through polarization direction withv1after No. four identical polaroids 55, frequency isv1,v2withv3the polarization laser of horizontal direction enter into No. six photodetectors 56 and change, its output electrical signals, its frequency isv1-v2,using this as bigness scale chi, and survey chi length is, another beam of laser through polarization direction withv1the electric signal that becomes to incide after No. five polaroids 59 of 45 degree 60 outputs of 60, No. five photodetectors of No. five photodetectors through low-pass filter filtering high frequency electrical signal, retain low frequency electric signal, its frequency isf1-f2, using this as accurate measurement chi, survey chi length is;
Step 5, by a phase detector 44 and No. two phase detectors 48, obtain respectively frequency and bev1-v2withf1-f2the phase differential of two path signalφ1withφ2, according to formulatry to achieve the distance measure of bigness scale chilc, and its substitution formula is tried to achieve to the phase place round values of accurate measurement chi; Whereinfloor(x) function returnsxthe integral part of value, finally according to formula, try to achieve tested distance value:, in formula: c is the light velocity, the air refraction that n is environment.
Described two path signal phase differentialφ1with phase differentialφ2measurement at synchronization, carry out.
Accurate measurement chi used and bigness scale chi all can be traced to the source.

Claims (6)

Translated fromChinese
1.一种基于可溯源同步测尺的混合双光源激光测距装置,包括扩束准直镜组(3),其特征在于:所述装置由测尺生成单元(1)、激光移频单元(2)、扩束准直镜组(3)和测量光路及电路单元(4)组成,测尺生成单元(1)发出的激光输出到激光移频单元(2)的输入端,激光移频单元(2)输出的一路激光通过扩束准直镜组(3)输出到测量光路及电路单元(4)的一个输入端,激光移频单元(2)输出的另一路激光直接输入到测量光路及电路单元(4)的另一个输入端;1. A hybrid dual light source laser distance measuring device based on a traceable synchronous measuring ruler, including a beam expanding collimating lens group (3), characterized in that: the device is composed of a measuring ruler generating unit (1), a laser frequency shifting unit (2), beam expander collimating lens group (3) and measuring optical path and circuit unit (4), the laser output from the ruler generating unit (1) is output to the input end of the laser frequency shifting unit (2), and the laser frequency shifts One laser output from the unit (2) is output to the measurement optical path and one input end of the circuit unit (4) through the beam expander collimating lens group (3), and the other laser output from the laser frequency shifting unit (2) is directly input to the measurement optical path and another input end of the circuit unit (4);所述测尺生成单元(1)的结构是:频率基准激光器(5)发射的激光束到达分光器(6)的输入端,分光器(6)的第一输出端连接二号分光镜(7)的一个输入端, 二号分光镜(7)的一个输出端连接一号光电探测器(9)的输入端,分光器(6)的第二输出端连接二号分光镜(8)的一个输入端,二号分光镜(8)的输出端连接二号光电探测器(10)的输入端,一号光电探测器(9)和二号光电探测器(10)的输出端连接单片机(11)的输入端,单片机(11)的两个输出端连接腔长调整执行器(12)的两个输入端,腔长调整执行器(12)的两个输出端分别连接半导体激光器(13)和双纵模He-Ne激光器(14)的输入端,半导体激光器(13)的一个输出端连接三号分光镜(15)的一个输入端,三号分光镜(15)的一个输出端连接一号反射镜(16)的输入端,一号反射镜(16)的输出端连接一号偏振片(17)的输入端,双纵模He-Ne激光器(14)的一个输出端连接二号分光镜(8)的一个输入端;The structure of the measuring ruler generating unit (1) is: the laser beam emitted by the frequency reference laser (5) reaches the input end of the beam splitter (6), and the first output end of the beam splitter (6) is connected to the second beam splitter (7 ), one output end of the second beam splitter (7) is connected to the input end of the first photodetector (9), and the second output end of the beam splitter (6) is connected to one of the second beam splitter (8) The input terminal, the output terminal of the second beam splitter (8) is connected to the input terminal of the second photodetector (10), and the output terminals of the first photodetector (9) and the second photodetector (10) are connected to the single chip microcomputer (11 ), the two output ends of the single chip microcomputer (11) are connected to the two input ends of the cavity length adjustment actuator (12), and the two output ends of the cavity length adjustment actuator (12) are respectively connected to the semiconductor laser (13) and The input end of the dual longitudinal mode He-Ne laser (14), an output end of the semiconductor laser (13) is connected to an input end of the No. 3 beam splitter (15), and an output end of the No. 3 beam splitter (15) is connected to the No. 1 The input end of the reflector (16), the output end of the first reflector (16) is connected to the input end of the first polarizer (17), and one output end of the dual longitudinal mode He-Ne laser (14) is connected to the second beam splitter (8) an input terminal;所述激光移频单元(2)的结构是:测尺生成单元(1)的一个输出端连接九号反射镜(35)的输入端,九号反射镜(35)的输出端连接三号分光镜(26)的一个输入端,三号分光镜(26)的输出端连接四号分光镜(36)的一个输入端,测尺生成单元(1)的另一个输出端连接一号偏振分光镜(18)的输入端,一号偏振分光镜(18)的一个输出端连接一号半波片(19)的输入端,一号半波片(19)的输出端连接二号偏振分光镜(20)的输入端,二号偏振分光镜(20)的一个输出端连接三号偏振分光镜(25)的一个输入端,二号偏振分光镜(20)的另一个输出端连接四号反射镜(21)的输入端,四号反射镜(21)的输出端连接一号激光移频器(23)的一个输入端,一号DDS信号源(22)的输出端连接一号激光移频器(23)的另一个输入端,一号激光移频器(23)的输出端连接五号反射镜(24)的输入端,五号反射镜(24)的输出端连接三号偏振分光镜(25)的另一个输入端,三号偏振分光镜(26)的输出端连接三号分光镜(26)的另一个输入端,三号分光镜(26)的输出端连接四号分光镜(36)一个输入端,一号偏振分光镜(18)的另一个输出端连接六号反射镜(27)的输入端,六号反射镜(27)的输出端经过二号半波片(28)连接四号偏振分光镜(29)的输入端,四号偏振分光镜(29)的一个输出端连接五号偏振分光镜(34)的一个输入端,四号偏振分光镜(29)的另一个输出端连接七号反射镜(30)的输入端,七号反射镜(30)的输出端连接二号激光移频器(32)的一个输入端,二号DDS信号源(31)的输出端连接二号激光移频器(32)的另一个输入端,二号激光移频器(32)的输出端连接八号反射镜(33)的输入端,八号反射镜(33)的输出端连接五号偏振分光镜(34)的另一个输入端,五号偏振分光镜(34)的输出端连接四号分光镜(36)的另一个输入端;The structure of the laser frequency shifting unit (2) is as follows: an output end of the ruler generation unit (1) is connected to the input end of the No. 9 reflector (35), and the output end of the No. 9 reflector (35) is connected to the No. One input end of the mirror (26), the output end of the third beam splitter (26) is connected to one input end of the fourth beam splitter (36), and the other output end of the ruler generating unit (1) is connected to the first polarizing beam splitter (18), an output end of the No. 1 polarizing beam splitter (18) is connected to the input end of the No. 1 half-wave plate (19), and the output end of the No. 1 half-wave plate (19) is connected to the No. 2 polarizing beam splitter ( 20), one output end of the second polarizing beam splitter (20) is connected to one input end of the third polarizing beam splitter (25), and the other output end of the second polarizing beam splitter (20) is connected to the fourth reflector The input terminal of (21), the output terminal of the fourth reflector (21) is connected to an input terminal of the No. 1 laser frequency shifter (23), and the output terminal of the No. 1 DDS signal source (22) is connected to the No. 1 laser frequency shifter The other input end of (23), the output end of No. 1 laser frequency shifter (23) is connected to the input end of No. 5 reflector (24), and the output end of No. 5 reflector (24) is connected to No. 3 polarization beam splitter ( 25), the output of No. 3 polarizing beam splitter (26) is connected to the other input of No. 3 beam splitter (26), and the output of No. 3 beam splitter (26) is connected to No. 4 beam splitter (36) ) one input end, the other output end of No. 1 polarizing beam splitter (18) is connected to the input end of No. 6 reflector (27), and the output end of No. 6 reflector (27) is connected through No. 2 half-wave plate (28) The input end of the No. 4 polarizing beam splitter (29), an output port of the No. 4 polarizing beam splitter (29) is connected to an input port of the No. 5 polarizing beam splitter (34), and another output of the No. 4 polarizing beam splitter (29) connected to the input of No. 7 reflector (30), the output of No. 7 reflector (30) to an input of No. 2 laser frequency shifter (32), and the output of No. 2 DDS signal source (31) to The other input end of the No. 2 laser frequency shifter (32), the output end of the No. 2 laser frequency shifter (32) is connected to the input end of the No. 8 reflector (33), and the output end of the No. 8 reflector (33) is connected to The other input end of the No. 5 polarizing beam splitter (34), the output end of the No. 5 polarizing beam splitter (34) is connected to the other input end of the No. 4 beam splitter (36);所述测量光路及电路单元(4)的结构是:激光移频单元(2)的一个输出端连接十二号反射镜(37)的输入端,十二号反射镜(37)的输出端连接五号反射镜(38)的输入端,五号反射镜(38)的一个输出端通过二号偏振片(39)与三号光电探测器(40)的输入端连通,三号光电探测器(40)的输出端连接一号低通滤波器(41)的输入端,一号低通滤波器(41)的输出端连接一号混频器(42)的一个输入端,三号DDS信号源(43)的一个输出端连接一号混频器(42)的另一个输入端,一号混频器(42)的输出端连接一号鉴相器(44)的一个输入端,五号反射镜(38)的另一个输出端通过三号偏振片(45)与四号光电探测器(46)的输入端连通,四号光电探测器(46)的输出端连接二号低通滤波器(47)的输入端,二号低通滤波器(47)的输出端连接二号鉴相器(48)的一个输入端,扩束准直镜组(3)的输出端连接六号偏振分光镜(49)的一个输入端,六号偏振分光镜(49)的一个输出端通过一号四分之一波片(50)与十号反射镜(51)的输入端连通,十号反射镜(51)的输出端通过一号四分之一波片(50)与六号偏振分光镜(49)的一个输入端连通,六号偏振分光镜(49)的一个输出端通过二号四分之一波片(52)与十一号反射镜(53)的输入端连通,十一号反射镜(53)的输出端通过二号四分之一波片(52)与六号偏振分光镜(49)的另一个输入端连通,六号偏振分光镜(49)的另一个输出端连接八号分光镜(54)的一个输入端,八号分光镜(54)的一个输出端通过四号偏振片(55)与五号光电探测器(56)的输入端连通,五号光电探测器(56)的输出端连接三号低通滤波器(57)的输入端,三号低通滤波器(57)的输出端连接三号混频器(58)的一个输入端,三号DDS信号源(43)的另一个输出端连接三号混频器(58)的另一个输入端,三号混频器(58)的输出端连接一号鉴相器(44)的另一个输入端,八号分光镜(54)的另一个输出端通过五号偏振片(59)与六号光电探测器(60)的输入端连通,六号光电探测器(60)的输出端连接四号低通滤波器(61)的输入端,四号低通滤波器(61)的输出端连接二号鉴相器(48)的另一个输入端。The structure of the measurement optical path and circuit unit (4) is: an output end of the laser frequency shifting unit (2) is connected to the input end of the No. 12 reflector (37), and the output end of the No. 12 reflector (37) is connected to The input end of No. 5 reflector (38), an output end of No. 5 reflector (38) communicates with the input end of No. 3 photodetector (40) through No. 2 polarizer (39), No. 3 photodetector ( The output terminal of 40) is connected to the input terminal of the No. 1 low-pass filter (41), the output terminal of the No. 1 low-pass filter (41) is connected to an input terminal of the No. 1 mixer (42), and the No. 3 DDS signal source One output end of (43) is connected to the other input end of No. 1 mixer (42), and the output end of No. 1 mixer (42) is connected to an input end of No. 1 phase detector (44), and No. 5 reflected The other output end of mirror (38) communicates with the input end of No. 4 photodetector (46) through No. 3 polarizer (45), and the output end of No. 4 photodetector (46) is connected with No. 2 low-pass filter ( 47), the output of the No. 2 low-pass filter (47) is connected to an input of the No. 2 phase detector (48), and the output of the beam expander and collimator group (3) is connected to the No. 6 polarization beam splitter One input end of (49), one output end of No. 6 polarizing beam splitter (49) communicates with the input end of No. 10 reflector (51) through No. 1 quarter-wave plate (50), and No. 10 reflector ( The output end of 51) communicates with an input end of the No. 6 polarizing beam splitter (49) through the No. A wave plate (52) communicates with the input end of No. 11 reflector (53), and the output end of No. 11 reflector (53) is connected with No. 6 polarizing beam splitter ( 49) is connected to the other input end, and the other output end of No. 6 polarizing beam splitter (49) is connected to one input end of No. Sheet (55) is connected with the input terminal of No. 5 photodetector (56), the output terminal of No. 5 photodetector (56) is connected with the input terminal of No. 3 low-pass filter (57), and No. 3 low-pass filter ( The output terminal of No. 57) is connected to one input terminal of No. 3 mixer (58), and the other output terminal of No. 3 DDS signal source (43) is connected to the other input terminal of No. 3 mixer (58). The output end of the frequency converter (58) is connected to the other input end of the No. 1 phase detector (44), and the other output end of the No. 8 beam splitter (54) is connected to the No. 6 photodetector ( 60) is connected to the input, the output of No. 6 photodetector (60) is connected to the input of No. 4 low-pass filter (61), and the output of No. 4 low-pass filter (61) is connected to No. 2 phase detector (48) the other input.2.根据权利要求1所述的基于可溯源同步测尺的混合双光源激光测距装置,其特征在于:所述激光移频单元(2)的一、二号激光移频器(23)、(32)包括声光移频器、电光移频器,且激光频率可以调节。2. The hybrid dual light source laser ranging device based on traceable synchronous measuring ruler according to claim 1, characterized in that: the first and second laser frequency shifters (23) of the laser frequency shifting unit (2), (32) It includes an acousto-optic frequency shifter and an electro-optic frequency shifter, and the laser frequency can be adjusted.3.根据权利要求1所述的基于可溯源同步测尺的混合双光源激光测距装置,其特征在于:所述测尺生成单元(1)中频率基准激光器(5)包括碘稳频激光器、飞秒激光频率梳激光器,且频率稳定度优于10-123. The hybrid dual light source laser ranging device based on a traceable synchronous measuring ruler according to claim 1, characterized in that: the frequency reference laser (5) in the measuring ruler generating unit (1) includes an iodine frequency stabilized laser, Femtosecond laser frequency comb laser, and the frequency stability is better than 10-12 .4.一种如权利要求1所述的基于可溯源同步测尺的混合双光源激光测距方法,其特征在于:具体步骤如下:4. A hybrid dual light source laser ranging method based on traceable synchronous ruler as claimed in claim 1, characterized in that: the specific steps are as follows:步骤一、开启频率基准激光器(5)、半导体激光器(13)、双纵模He-Ne激光器(14),在经过预热和稳频之后,通过反馈控制,将半导体激光器(13)和双纵模He-Ne激光器(14)输出频率锁定在频率基准激光器(5)的一定频率范围之内,半导体激光器(13)输出频率经过一号偏振片(17),调整偏振角度使得只让频率为v1的激光通过,双纵模He-Ne激光器(14)输出频率为v2和v3的双频激光;Step 1. Turn on the frequency reference laser (5), the semiconductor laser (13), and the dual longitudinal mode He-Ne laser (14). After preheating and frequency stabilization, the semiconductor laser (13) and the dual longitudinal mode The output frequency of the mode He-Ne laser (14) is locked within a certain frequency range of the frequency reference laser (5), the output frequency of the semiconductor laser (13) passes through the No. 1 polarizer (17), and the polarization angle is adjusted so that only the frequency isv1 laser passes through, and the dual longitudinal mode He-Ne laser (14) outputs dual-frequency lasers with frequencies v2 and v3 ;步骤二、由步骤一所形成的三种频率的激光进入激光移频单元(2),其中一束双频激光用一号偏振分光镜(18)分出频率为v2v3两束激光,经过半波片之后再分别用二号偏振分光镜(20)和四号偏振分光镜(29)分出两束双频激光,其中一路经过激光移频器,由DDS信号源驱动激光移频器,频率分别为f1f2,最后各种频率的激光合并,其中共有五种频率,分别为v1v2 、v3 、v2+ f1 和v3+ f2,,这束激光入射到分光棱镜分为两束光,一束作为参考激光束,另一束作为测量激光束出射到测量目标;Step 2. The lasers of three frequencies formed in step 1 enter the laser frequency shifting unit (2), and one of the dual-frequency lasers is split into two laser beams with frequenciesv2 andv3 by the No. 1 polarizing beam splitter (18) , after passing through the half-wave plate, use the No. 2 polarizing beam splitter (20) and the No. 4 polarizing beam splitter (29) to separate two beams of dual-frequency lasers, one of which passes through the laser frequency shifter, and the laser frequency shift is driven by the DDS signal source , the frequencies aref1 andf2 , and finally the lasers of various frequencies are combined, and there are five frequencies in total, namelyv1 ,v2 ,v3 ,v2 +f1 andv3 +f2, which A beam of laser light enters the beam splitting prism and is divided into two beams of light, one beam is used as a reference laser beam, and the other beam is used as a measurement laser beam to exit to the measurement target;步骤三、参考激光束经分光棱镜分为两束激光束,一束激光束经偏振方向与v1相同的二号偏振片(39)后,频率为v1v2 和v3的水平方向的偏振激光进入到三号光电探测器(40)进行转换,其输出电信号,其频率为v1-v2,以此作为粗测尺,另一束激光经偏振方向与v1成45度的三号偏振片(45)后入射到四号光电探测器(46),四号光电探测器(46)输出的电信号经过低通滤波器滤除了高频电信号,保留低频电信号,其频率为f1-f2,以此作为精测尺;Step 3, the reference laser beam is divided into two beams of laser beams by a beam splitter, and the frequency of one laser beam is the horizontal direction ofv1 ,v2 andv3 after passing through the No.2 polarizer (39) with the same polarization direction asv 1 The polarized laser light enters the No. 3 photodetector (40) for conversion, and its output electrical signal has a frequency ofv1 -v2, which is used as a rough measuring scale. The polarization direction of the other beam of laser light is 45 degrees tov1 The No. 3 polarizer (45) is incident on the No. 4 photodetector (46), and the electrical signal output by the No. 4 photodetector (46) is filtered by a low-pass filter to remove the high-frequency electrical signal, and retains the low-frequency electrical signal. The frequency isf1 -f2 , which is used as a precise measuring stick;步骤四、测量开始时,参考面十号反射镜(51)固定不动,移动十一号反射镜(53)至目标端,测量距离为L,测量光束经测量反射镜(53)反射后,与参考面反射回来的光束在六号偏振分光镜(49)处汇聚,进入测量电路,测量激光束经分光棱镜分为两束激光束,其中一束激光束经偏振方向与v1相同的四号偏振片(55)后,频率为v1v2 和v3的水平方向的偏振激光进入到六号光电探测器(56)进行转换,其输出电信号,其频率为v1-v2,以此作为粗测尺,测尺长为                                                ,另一束激光经偏振方向与v1成45度的五号偏振片(59)后入射到五号光电探测器(60),五号光电探测器(60)输出的电信号经过低通滤波器滤除了高频电信号,保留低频电信号,其频率为f1-f2,以此作为精测尺,测尺长为Step 4. When the measurement starts, the No. 10 reflector (51) on the reference surface is fixed, and the No. 11 reflector (53) is moved to the target end. The measurement distance is L. After the measurement beam is reflected by the measurement reflector (53), The light beam reflected back from the reference surface converges at No. 6 polarizing beam splitter (49) and enters the measurement circuit. The measuring laser beam is divided into two laser beams throughthebeam splitting prism. After the No. polarizer (55), the horizontally polarized laser light with frequencies ofv1 ,v2 andv3 enters the No. 6 photodetector (56) for conversion, and its output electric signal has a frequency ofv1 -v2, as a rough measuring ruler, the length of the measuring ruler is , another beam of laser light is incident on the No. 5 photodetector (60) after the No. 5 polarizer (59) whose polarization direction is 45 degrees withv1 , and the electric signal output by No. 5 photodetector (60) is low-pass filtered The filter filters out the high-frequency electrical signal and retains the low-frequency electrical signal. Its frequency isf1 -f2 , and it is used as a precise measuring ruler. The length of the measuring ruler is ;步骤五、由一号鉴相器(44)和二号鉴相器(48)分别得到频率为v1-v2f1-f2的两路电信号的相位差φ1φ2,根据公式求得粗测尺的距离测量值Lc,并将其代入公式求得精测尺的相位整数值;其中floor(x)函数返回x值的整数部分,最后根据公式求得被测距离值:,式中:c为光速,n为环境的空气折射率。Step 5, obtain the phase difference φ 1andφ 2 of the two-way electric signal that frequency isv1 -v2 andf1 -f2 byNo. 1 phase detector (44) and No. 2phase detector (48), According to the formula Obtain the distance measurement valueLc of the coarse measuring ruler, and substitute it into the formula to obtain the phase integer value of the fine measuring ruler ; wherethe floor (x ) function returns the integer part ofthe x value, and finally obtains the measured distance value according to the formula: , where: c is the speed of light, and n is the refractive index of the ambient air.5.根据权利要求4所述的基于可溯源同步测尺的混合双光源激光测距方法,其特征在于:所述两路电信号相位差与相位差的测量在同一时刻进行。5. The hybrid dual light source laser ranging method based on traceable synchronous measuring ruler according to claim 4, characterized in that: the phase difference of the two electrical signals and phase difference measurements are performed at the same time.6.根据权利要求4所述的基于可溯源同步测尺的混合双光源激光测距方法,其特征在于:所用精测尺与粗测尺均可溯源。6. The hybrid dual light source laser ranging method based on a traceable synchronous measuring ruler according to claim 4, characterized in that: both the fine measuring ruler and the coarse measuring ruler used are traceable.
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