CN1233759A - Incoherent laser radar system atmospheric sounding - Google Patents

Incoherent laser radar system atmospheric sounding Download PDF

Info

Publication number
CN1233759A
CN1233759A CN98110798A CN98110798A CN1233759A CN 1233759 A CN1233759 A CN 1233759A CN 98110798 A CN98110798 A CN 98110798A CN 98110798 A CN98110798 A CN 98110798A CN 1233759 A CN1233759 A CN 1233759A
Authority
CN
China
Prior art keywords
fabry
perot interferometer
laser
light beam
radar system
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN98110798A
Other languages
Chinese (zh)
Other versions
CN1089443C (en
Inventor
胡企铨
张哨峰
陆雨田
甘柏辉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Institute of Optics and Fine Mechanics of CAS
Original Assignee
Shanghai Institute of Optics and Fine Mechanics of CAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanghai Institute of Optics and Fine Mechanics of CAS filed Critical Shanghai Institute of Optics and Fine Mechanics of CAS
Priority to CN98110798A priority Critical patent/CN1089443C/en
Publication of CN1233759A publication Critical patent/CN1233759A/en
Application granted granted Critical
Publication of CN1089443C publication Critical patent/CN1089443C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Landscapes

  • Optical Radar Systems And Details Thereof (AREA)

Abstract

A incoherent laser radar system is mainly used for searching the wind velocity, aerosol density and cloud layer heightness of atmosphere. It contains single frequency laser, the laser beam passes through acoustooptic modulator to produce two light beam Gb and Gt, light baem Gt is passed through amplifier, optical unidirectional element, and is ejected from scanning optical element to atmosphere target, the signal light Gb reflected back from target is collected by receiving transmitting element and passes through unidirectional element, enters into servo controlled cofocal structure Fabry-Perot interferometer with light beam Gh to photoelectric detector and data collecting processor. Its characteristics include simple, high receiving efficiency and signal-to-noise ratio simple and convenient in signal data processing.

Description

The incoherent laser radar system of atmospheric sounding
The present invention relates to a kind of laser radar system of atmospheric sounding, particularly relate to the laser radar system that adopts non-coherent approaches to measure the atmosphere wind speed.Be mainly used in wind speed, aerosol density and the ceiling of clouds etc. of atmospheric sounding.
It is the Doppler shift that utilizes continuous laser that laser radar is surveyed wind speed, adopts the optical heterodyne technology to realize.Its principle is: the wind speed of the group velocity of big molecule of gasoloid or suspended particulates reflection atmosphere in the atmosphere, they cause the Doppler shift υ of rear orientation light dWind speed V and Doppler shift υ along radiation direction dRelation is arranged:
υ d=2V/λ
If do light source with solid (YAG) laser instrument, λ=1.06 μ m then has υ d=1.89MHz/ (m/s).Measure Doppler shift, just can calculate radially wind speed along radiation direction.
Prior art 1:
[Coherent launch-site atmospheric wind sounder:theory and experiment.James G.Hawley as shown in Figure 1, Russell Targ, Sammy W.Henderson, Charley P.Hale, Michael J.Kavaya, and Daniel Moerder, Appl.Opt.32,4557-4568 (1993)].Its detection system is the output beam G of a continuous single-frequency laser 1 bAs the local oscillation source, its frequency is υ l, another Shu Guangjing amplifier 2 pulses are amplified the back as detecting light beam G tThrough the transmitting-receiving optical module 4 directive atmosphere targets of an optical-unidirectional device 3 from having scanning monitor 8.By the light signal generating Doppler shift that target reflection is returned, frequency is υ l+ υ dEcho beam G hThrough transmitting-receiving optical module 4 and isolator 3, by coupling mechanism 5 and the mixing in photodetector 6 of local oscillation source, the difference frequency signal of gained is Doppler shift υ dThis signal is handled by data collection processor 7, can obtain the numerical value of atmosphere wind speed.
This system is limited in: its corrugated of the flashlight that target reflection is returned can produce distortion, adds the influence of transmitting-receiving optical module acceptance angle, and mixing efficiency is low, influences signal to noise ratio (S/N ratio) and operating distance.
Prior art 2:
As shown in Figure 2.[A?simple?two?component?laser?Doppler?anemometer?using?a?rotatingdiffraction?grating,J.Oldengarm?&?Prabha?Venkatesh,J.Phys.E.Sci.Instr.9,1009-1012(1976)]。Its detection system is the output of a continuous wave laser 1, after frequency modulation (PFM), pass through beam splitter 10 beam splitting with a rotating grating 9, generally be in orthogonal form again through transmitting-receiving optical module 4 directive targets with four bundle light, the signal of being returned by target reflection receives through transmitting-receiving optical module 4, obtains to interfere in twos between light beam the doppler shifted signal that produces in photodetector 6.This signal is handled by data collection processor 7, can obtain target velocity.
This system is limited in: the power of continuous wave laser is low, and the light path layout of instrument requires to intersect at the target area light beam, so operating distance is very short.
In order to overcome the restriction of said system, once developed a kind of incoherent pulses Doppler speed measuring laser radar.The key distinction of it and coherent Doppler laser radar system is to survey Doppler shift and does not adopt the optical heterodyne technology.
Prior art 3:
[Observation of winds with an incoherent lidar detector, Vincent J.Abreu, John Barnes, and Paul B.Hays, Appl.Opt.31,4509-4514 (1992)] as shown in Figure 3.The Laser emission structure is similar with prior art 1 basically.Receiving unit is in order to realize the Doppler shift with noncoherent detection of a target echo, adopts that a fixed flat planar Fabry--perot interferometer 11 is made high-resolution light filter.6 of photodetectors need to adopt a kind of bidimensional hyperchannel image light electric explorer, so that detect at least one complete Fabry--the echo in the perot interferometer free spectral range, then detectable signal is delivered to data collection processor 7 and handled, obtain target velocity.
This system is limited in: the fixed flat planar Fabry--perot interferometer is made high-resolution light filter, has limited the reception visual field owing to adopt in the receiving unit; Because of dull and stereotyped Fabry--in the output of perot interferometer high-order component is arranged, even adopt bidimensional hyperchannel image light electric explorer, the signal that detects also is a complete Fabry--the echo in the perot interferometer free spectral range usually, this only is the part of received signal, influences also influence distance of receiving efficiency; And used bidimensional multi channel imaging photodetector is a kind of relatively more expensive optoelectronic component, and two-dimensional signal is handled also more complicated.
In order to solve the incoherent laser radar problem of the Doppler shift of detection of a target echo effectively, people have done many work, some imaginations that may deal with problems have been proposed, for example adopting the sphere Fabry--the absorption line of perot interferometer, atom or molecule is as [Edge technique:theory and application tothe lidar measurement of atmospheric wind such as high-resolution light filters, C.Laurence Korb, Bruce M.Gentry, and Chi Y.Weng, Appl.Opt.31,4202-4213 (1992)].
The objective of the invention is to propose incoherent laser radar system in order to overcome the difficulty of existed system 1-3, butt joint rating field has no particular limits, and can improve receiving efficiency and signal to noise ratio (S/N ratio).Frequency and light intensity fluctuation to laser output are insensitive.Requirement to photodetector 6 is not harsh, can use bidimensional multi channel imaging photodetector, and signal data is handled easy.Both the atmosphere wind speed can be measured, parameters such as atmospheric density and ceiling of clouds can also be measured.
System architecture of the present invention as shown in Figure 4.Contain a continuous single-frequency main oscillations laser instrument 1, the light beam of output produces two bundle frequency and all different light beam G of time waveform through 12 modulation of an acousto-optic modulator b, G tWherein a branch of G bBe continuous light beam, send into Fabry--the perot interferometer 14 of band servo controller 13, as control Fabry--the frequency standard light beam that the perot interferometer resonant cavity is long.Another light beam G t, its intensity is amplified by amplifier 2 after the modulation of the time of acousto-optic modulator 12, as detecting light beam G tThrough an optical-unidirectional device 3 from transmitting-receiving optical module 4 directive atmosphere targets.Light beam G bWith light beam G tDifference on the frequency be acoustooptic modulation frequency υ ΩThe signal beams G that returns by target reflection hCollect through transmitting-receiving optical module 4,, enter servo-controlled Fabry by isolator 3--perot interferometer 14, to survey by photodetector 6, the signal that measures is deeply sent in the data collection processor 7 and is handled.Work as Fabry--perot interferometer is got confocal arrangement, and as shown in Figure 4, the relation between its transmitance and incident optical frequency is as shown in Figure 5.
Confocal Fabry--perot interferometer 14, it is made of two spherical mirrors 141,142 that common focus O is arranged and piezoelectric ceramics 143.Between two spherical mirrors 141 and 142 is the clearance, and spacing is L, and two confocal spherical mirrors 141 and 142 reflectivity are respectively R, and then when optical maser wavelength was λ, the strength ratio of transmission and incident was:
I T/I o={1+4R?Sin 2(δ/2)/(1-R2)} -1
δ=4 π L/ λ wherein.I o-be incident intensity, I T-be transmitted light intensity, the band width of this Fabry--perot interferometer free spectral range is: △ υ=C/4L.The half width of transmission maximum is: Δω 1 / 2 = C ( 1 - R ) / L R
F ≈ π R / ( 1 - R ) , F is called Fabry again--and the acutance coefficient of perot interferometer, R is relevant for it and Fabry--perot interferometer face specular reflectivity.If Fabry--perot interferometer spacing L=50 millimeter, about 1.5 kilo-mega cycles per seconds of the band width of its free spectral range, (R ≈ 0.8), then △ (ω when F ≈ 30 1/2≈ 50 megahertzes.
If the peak that sees through of confocal Fabry--perot interferometer is locked in light beam G by servocontrol bFrequency υ GbThe place, as shown in Figure 5.Detecting light beam G tFrequency υ GtBe positioned at the half waist △ ω that this sees through the peak, the light signal of being returned, had Doppler shift by the atmospheric wind target reflection is through confocal Fabry--during perot interferometer, its output intensity will become with Doppler shift.Measure this variation, handle, then can obtain the wind field data of atmosphere by signal data acquisition processor 7.
Advantage of the present invention:
(1) because of receiving system is the high resolving power light filter with servo-controlled confocal Fabry-Perot interferometer 14, so laser radar system of the present invention butt joint rating field has no particular limits, it has higher receiving efficiency and signal to noise ratio (S/N ratio).
(2) laser radar system of the present invention is to be divided into two light beams G by the laser beam that laser instrument 1 is exported behind acousto-optic modulator 12 b, G tWherein a branch of is continuous light beam G b, servo-controlled confocal Fabry-Perot interferometer is locked in G bOn, so be applicable to the laser of any wavelength, and insensitive to laser output frequency and light intensity fluctuation.
(3) laser radar system of the present invention and prior art 3 ratios are not harsh to the requirement of photodetector 6, can use bidimensional multi channel imaging photodetector, and signal data is handled easy.
(4) laser radar system of the present invention both can be measured the atmosphere wind speed, can measure other atmospheric parameters such as atmospheric density and ceiling of clouds again.
Description of drawings:
Fig. 1: be the laser radar system synoptic diagram of prior art 1 atmospheric sounding.
Fig. 2: be the laser velocimeter system synoptic diagram of prior art 2.
Fig. 3: be the laser radar system synoptic diagram of prior art 3 atmospheric soundings.
Fig. 4: be the incoherent laser radar system synoptic diagram of atmospheric sounding of the present invention.
The transmitance of Fig. 5: be confocal Fabry--perot interferometer and the graph of a relation between the incident light frequency, wherein, horizontal ordinate is beam frequencies υ, ordinate is any luminous intensity unit I.
Embodiment:
As shown in Figure 4, a continuous single-frequency laser 1, the light beam of output produces two bundle frequency and all different main oscillations light beam of time waveform G through 12 modulation of an acousto-optic modulator b, G tWherein a branch of is continuous light beam G b, send into Fabry--the perot interferometer 14 of being with servo controller 13, as the Fabry of control--the frequency standard light beam that the perot interferometer resonant cavity is long.Another light beam G t, its intensity is amplified by amplifier 2 after the time modulation, as detecting light beam G tThrough an optical-unidirectional device 3 from transmitting-receiving optical module 4 directive atmosphere targets.The flashlight G that returns by target reflection hCollect through transmitting-receiving optical module 4,, enter servo-controlled Fabry by isolator 3--perot interferometer 14, survey by photodetector 6.For each device of layout reasonably, in the light path of Fig. 4, add saturating anti-mirror M t, mirror M 2, M 3, and prism P 1, P 2Servo controller 13 is to be made of the piezoelectric ceramics that photodetection and electronic circuit are controlled.Fabry--perot interferometer 14 is confocal arrangement, its clearance spacing L=30 millimeter, and two confocal spherical mirror reflectivity are respectively R=0.8, during laser wavelength lambda=0.53 micron, the strength ratio I of transmission and incident T/ I O≈ 10%.The band width of this Fabry--perot interferometer free spectral range is △ υ=2.5 kilo-mega cycles per seconds, (R ≈ 0.8), then △ ω when F ≈ 15 1/2≈ 160 megahertzes are as acoustooptic modulation frequency υ ΩWhen being 80 megahertzes, detecting light beam G tFrequency just in time be positioned at Fabry--perot interferometer sees through half waist at peak, as shown in Figure 5.
The light signal that Doppler shift is arranged by the backspace of atmospheric wind target is through confocal Fabry--during perot interferometer, its output intensity will become with Doppler shift.Measure this variation, handle, just can obtain the wind field data of atmosphere by signal data acquisition processor 7.

Claims (2)

1. the incoherent laser radar system of an atmospheric sounding contains
(1) continuous single-frequency laser (1), output two-beam G b, G t,
(2) along light beam G tOn the direction of advancing, be equipped with amplifier (2) successively, optical-unidirectional device (3) and transmitting-receiving optical module (4);
(3) along light beam G bOn the direction of advancing, Fabry-Perot interferometer (14) is arranged;
(4) facing to Fabry--perot interferometer (14) output terminal is equipped with photodetector (6);
(5) output of photodetector (6) is connected in data collection processor (7);
(6) data collection processor spare (7) links to each other with the scanning monitor (8) of transmitting-receiving optical device (4);
It is characterized in that:
(7) place between laser instrument (1) and the amplifier (2) acousto-optic modulator (12) is arranged, the output beam of laser instrument (1) is divided into two-beam G afterwards through acousto-optic modulator (12) b, G t
(8) Fabry--perot interferometer (14) is a confocal arrangement, has servo controller (13).
2. according to the laser radar system of claim 1, it is characterized in that servo-controlled Fabry-Perot interferometer (14) is by two spherical mirrors (141) that common focus O is arranged and (142), and the confocal arrangement of piezoelectric ceramics (143) formation.
CN98110798A 1998-04-24 1998-04-24 Incoherent laser radar system atmospheric sounding Expired - Fee Related CN1089443C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN98110798A CN1089443C (en) 1998-04-24 1998-04-24 Incoherent laser radar system atmospheric sounding

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN98110798A CN1089443C (en) 1998-04-24 1998-04-24 Incoherent laser radar system atmospheric sounding

Publications (2)

Publication Number Publication Date
CN1233759A true CN1233759A (en) 1999-11-03
CN1089443C CN1089443C (en) 2002-08-21

Family

ID=5220816

Family Applications (1)

Application Number Title Priority Date Filing Date
CN98110798A Expired - Fee Related CN1089443C (en) 1998-04-24 1998-04-24 Incoherent laser radar system atmospheric sounding

Country Status (1)

Country Link
CN (1) CN1089443C (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1329742C (en) * 2004-09-30 2007-08-01 中国科学院安徽光学精密机械研究所 Laser radar control method based on image intensifier
CN100365434C (en) * 2001-02-09 2008-01-30 联邦科学及工业研究组织 Lidar system and method
CN101852855B (en) * 2005-02-14 2012-07-18 数字信号公司 Laser radar system and system and method for providing chirped electromagnetic radiation
CN102053048B (en) * 2009-11-09 2012-07-25 中国气象科学研究院 Dynamic aerosol wind tunnel detection system
CN101341421B (en) * 2005-12-20 2013-03-27 皇家飞利浦电子股份有限公司 Device and method for measuring relative movement
CN101918811B (en) * 2007-10-25 2013-07-31 圣路易斯华盛顿大学 Confocal photoacoustic microscopy with optical lateral resolution
CN103424749A (en) * 2012-05-22 2013-12-04 杨少辰 Full-optical-fiber laser radar visibility meter
CN103499820A (en) * 2013-09-27 2014-01-08 中国科学技术大学 All-fiber direct detection anemometric laser radar system and closed-loop control method thereof
JP2017049243A (en) * 2015-09-02 2017-03-09 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ Remote target identification using laser doppler vibrometry
CN109154663A (en) * 2016-02-26 2019-01-04 密歇根宇航公司 For directly detecting the multicomponent Fabry-Perot etalon interferometer of laser radar

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100365434C (en) * 2001-02-09 2008-01-30 联邦科学及工业研究组织 Lidar system and method
CN1329742C (en) * 2004-09-30 2007-08-01 中国科学院安徽光学精密机械研究所 Laser radar control method based on image intensifier
CN101852855B (en) * 2005-02-14 2012-07-18 数字信号公司 Laser radar system and system and method for providing chirped electromagnetic radiation
CN101341421B (en) * 2005-12-20 2013-03-27 皇家飞利浦电子股份有限公司 Device and method for measuring relative movement
CN101918811B (en) * 2007-10-25 2013-07-31 圣路易斯华盛顿大学 Confocal photoacoustic microscopy with optical lateral resolution
CN102053048B (en) * 2009-11-09 2012-07-25 中国气象科学研究院 Dynamic aerosol wind tunnel detection system
CN103424749A (en) * 2012-05-22 2013-12-04 杨少辰 Full-optical-fiber laser radar visibility meter
CN103424749B (en) * 2012-05-22 2015-08-19 深圳大舜激光技术有限公司 A kind of Full-optical-fiber laser radar visibility meter
CN103499820A (en) * 2013-09-27 2014-01-08 中国科学技术大学 All-fiber direct detection anemometric laser radar system and closed-loop control method thereof
JP2017049243A (en) * 2015-09-02 2017-03-09 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ Remote target identification using laser doppler vibrometry
CN109154663A (en) * 2016-02-26 2019-01-04 密歇根宇航公司 For directly detecting the multicomponent Fabry-Perot etalon interferometer of laser radar

Also Published As

Publication number Publication date
CN1089443C (en) 2002-08-21

Similar Documents

Publication Publication Date Title
CA2722603C (en) Laser doppler velocimeter
US5847817A (en) Method for extending range and sensitivity of a fiber optic micro-doppler ladar system and apparatus therefor
CN100578261C (en) Continuous wave frequency adjustment coherent optical fiber laser radar
US5510890A (en) Laser radar with reference beam storage
US4995720A (en) Pulsed coherent Doppler laser radar
EP1144982B1 (en) Speckle mitigation for coherent detection employing a wide band signal
US20200371239A1 (en) 360 degrees field of view scanning lidar with no movable parts
CN110133616B (en) Laser radar system
CN1089443C (en) Incoherent laser radar system atmospheric sounding
US4875770A (en) Wind shear detector
CN109991623A (en) A kind of distribution type laser radar
CN109991622A (en) A kind of laser radar
CN1831561A (en) Chaos laser range-meaurement device and method of LD pumping solid laser
US7450222B1 (en) Correlated-intensity velocimeter for arbitrary reflector
EP0477888B1 (en) System for the detection of the position and orientation of an object in space
CN111948665A (en) Solid-state laser radar system and solid-state laser radar
Meyzonnette et al. Imaging CO2 laser radar A comparison of three techniques: LFM pulse compression, FMCW, CW
Berkovic et al. Wavelength-modulated fiber optic sensor for high precision displacement measurement
CN212207680U (en) Laser radar system
Agishev Analytic comparison of some features of pulse-lidar and CW-FM-ladar remote sensing
GB2108348A (en) Doppler lidar
CN117214871A (en) Optical transceiver module and laser radar
Bartolini et al. Coherent laser sensor for robotic applications
Olsson et al. 1.55-m Multifunction Laser Radar using Fibre Optic Components
NZ230261A (en) Laser doppler velocimeter for detection of wind velocity gradient

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee