EP1886166A1 - Verfahren zum messen der luftgeschwindigkeit mit einem doppler-radar - Google Patents

Verfahren zum messen der luftgeschwindigkeit mit einem doppler-radar

Info

Publication number
EP1886166A1
EP1886166A1 EP06755534A EP06755534A EP1886166A1 EP 1886166 A1 EP1886166 A1 EP 1886166A1 EP 06755534 A EP06755534 A EP 06755534A EP 06755534 A EP06755534 A EP 06755534A EP 1886166 A1 EP1886166 A1 EP 1886166A1
Authority
EP
European Patent Office
Prior art keywords
speed
calculate
nyquist
rates
velocity
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.)
Withdrawn
Application number
EP06755534A
Other languages
English (en)
French (fr)
Inventor
Pierre Tabary
Laurent Perier
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.)
METEO-FRANCE
METEO FRANCE
Original Assignee
METEO-FRANCE
METEO FRANCE
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 METEO-FRANCE, METEO FRANCE filed Critical METEO-FRANCE
Publication of EP1886166A1 publication Critical patent/EP1886166A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • G01S13/95Radar or analogous systems specially adapted for specific applications for meteorological use
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/06Systems determining position data of a target
    • G01S13/08Systems for measuring distance only
    • G01S13/10Systems for measuring distance only using transmission of interrupted, pulse modulated waves
    • G01S13/22Systems for measuring distance only using transmission of interrupted, pulse modulated waves using irregular pulse repetition frequency
    • G01S13/227Systems for measuring distance only using transmission of interrupted, pulse modulated waves using irregular pulse repetition frequency with repetitive trains of uniform pulse sequences, each sequence having a different pulse repetition frequency
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/50Systems of measurement based on relative movement of target
    • G01S13/58Velocity or trajectory determination systems; Sense-of-movement determination systems
    • G01S13/581Velocity or trajectory determination systems; Sense-of-movement determination systems using transmission of interrupted pulse modulated waves and based upon the Doppler effect resulting from movement of targets
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/50Systems of measurement based on relative movement of target
    • G01S13/52Discriminating between fixed and moving objects or between objects moving at different speeds
    • G01S13/522Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves
    • G01S13/524Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi
    • G01S13/53Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi performing filtering on a single spectral line and associated with one or more range gates with a phase detector or a frequency mixer to extract the Doppler information, e.g. pulse Doppler radar
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/50Systems of measurement based on relative movement of target
    • G01S13/58Velocity or trajectory determination systems; Sense-of-movement determination systems
    • G01S13/581Velocity or trajectory determination systems; Sense-of-movement determination systems using transmission of interrupted pulse modulated waves and based upon the Doppler effect resulting from movement of targets
    • G01S13/582Velocity or trajectory determination systems; Sense-of-movement determination systems using transmission of interrupted pulse modulated waves and based upon the Doppler effect resulting from movement of targets adapted for simultaneous range and velocity measurements
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • G01S13/95Radar or analogous systems specially adapted for specific applications for meteorological use
    • G01S13/951Radar or analogous systems specially adapted for specific applications for meteorological use ground based
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/28Details of pulse systems
    • G01S7/285Receivers
    • G01S7/292Extracting wanted echo-signals
    • G01S7/2923Extracting wanted echo-signals based on data belonging to a number of consecutive radar periods
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/10Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Definitions

  • the present invention relates to "a method of measuring the air velocity in a region of the atmosphere.
  • the radar transmits sinusoidal wave trains or pulses which are returned to the radar by particles suspended in the air; if the air has a movement causing the particles to move away from or towards the radar, the pulses returned to the radar have a phase shift with respect to the pulses emitted, an offset which makes it possible to calculate the radial velocity of the particles relative to the radar and therefore the speed of the air that carries them.
  • the speed can thus be determined without ambiguity if the real speed of the particles is within a so-called Nyquist interval depending on the rate of emission of the pulses (also called emission frequency).
  • the calculated velocity is equal to the actual velocity modulo the width of the Nyquist interval.
  • drawbacks in particular a strong solicitation of the transmitter, a significant consumption of the latter and a reduction in the range of the radar.
  • a method for measuring the air velocity in a Doppler zone of the atmosphere by means of a radar comprising the steps of:
  • each pulse is emitted at a rate different from that of subsequent pulses.
  • the Nyquist interval is obtained by combining the three emission rates so that the Nyquist interval is relatively wide. The pulses at the three emission rates are emitted successively to the same zone of the atmosphere, which limits the imprecision of the process.
  • the calculation of the velocity V of the air comprises the phases of:
  • the method comprises a step of determining the rates
  • V neq ppcm (p, r) * V n i
  • This mode of determination is relatively simple, reliable and fast.
  • the method comprises the step to assign to the speeds V 1 ', V 2 ' and V 3 ', before their use in the calculations, a noise corresponding to the noise specific to the radar and to the usual atmospheric conditions in the measuring zone and the step of folding the speeds V 1 ', V 2 ' and V 3 'and noisy in the intervals [-Vm, Vm] / [-V n2 , V 112 ] and [-V n3 , V n3 ] to obtain the speeds V 1 ', V 2 'and V 3 ' used later in the calculations.
  • FIG. 1 is a block diagram illustrating the general course of the process of the invention
  • FIG. 2 is a block diagram illustrating the progress of the frequency determination step according to the invention
  • FIG. 3 is a diagram illustrating the emission of pulses over time.
  • the method according to the invention is implemented by means of a Doppler radar capable of emitting pulses of pulses by changing the transmission rate between each pulse. .
  • the method of the invention starts with the step of emitting gusts of three pulses 1, 2, 3 at different rates F 1 , F 2 , F 3 (the duration t1 separating the pulses 1 and 2 is different from the duration t2 separating the pulses 2 and 3 and the duration t3 separating the pulse 3 from a burst of the pulse 1 of the following burst is also different from the times t1 and t2, see Figure 3).
  • step 40 for determining the velocities V 1 , V 2 , V 3 of the air from the pulses received in return from the pulses 1, 2, 3 of each burst.
  • the speed V of the air is then calculated from the speeds V 1 , V 2 , V 3 determined for the pulses received in return for each burst (step 50).
  • step 60 the average quadratic differences obtained for all the values of k are compared with each other and the speed V te st corresponding to the smallest mean square deviation is selected as the speed V of the air (step 60).
  • the step 10 for determining the rates Fi, F 2 , F 3 is detailed in FIG. 2 and begins with a phase 11 for determining pairs of parameter ratios p / q and r / s which will be used to define the rates F 2 , F 3 according to Fi.
  • constraints are imposed in the choice of the parameters p, q, r, s:
  • q and s are greater than p and r respectively, p / q is greater than r / s,
  • r is greater than s / 2.
  • the parameters p and r are advantageously greater than q / 2 and s / 2 respectively, to prevent the rates F 2 and F 3 are much lower than the rate F 1 , which may cause wear magnetron radar.
  • the parameter q is preferably equal to p + 1.
  • the step of determining the pulse emission rates continues with a phase 12 during which the selection of a first rate F 1 depends on the technical characteristics of the radar and the calculation of a Nyquist velocity V nl. corresponding.
  • a noise corresponding to the noise specific to the radar and the usual atmospheric conditions in the measurement zone is assigned to the speed V 1 'and the velocity V 1 ' thus noisy is folded as before in the range [- Vm / V nl ] to obtain the speed V 1 'used later in the calculations.
  • the noise added to the speed V 1 1 is a Gaussian distribution noise of zero average and standard deviation parameterizable so that this noise corresponds to that encountered under conditions of use.
  • the step of determining the pulse transmission rates is completed by comparing the test speeds V obtained for all the couples and the speed V to select the best torque.
  • the frequency determination method can be carried out for several noise levels in order to evaluate the relevance of the selected pairs with respect to the noise levels encountered.

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • General Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Radar Systems Or Details Thereof (AREA)
EP06755534A 2005-06-02 2006-05-30 Verfahren zum messen der luftgeschwindigkeit mit einem doppler-radar Withdrawn EP1886166A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0505607A FR2886737B1 (fr) 2005-06-02 2005-06-02 Procede de mesure de la vitesse de l'air par radar doppler
PCT/FR2006/001220 WO2006129006A1 (fr) 2005-06-02 2006-05-30 Procede de mesure de la vitesse de l'air par radar doppler

Publications (1)

Publication Number Publication Date
EP1886166A1 true EP1886166A1 (de) 2008-02-13

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP06755534A Withdrawn EP1886166A1 (de) 2005-06-02 2006-05-30 Verfahren zum messen der luftgeschwindigkeit mit einem doppler-radar

Country Status (4)

Country Link
US (1) US7579977B2 (de)
EP (1) EP1886166A1 (de)
FR (1) FR2886737B1 (de)
WO (1) WO2006129006A1 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2886737B1 (fr) * 2005-06-02 2007-09-07 Meteo France Etablissement Pub Procede de mesure de la vitesse de l'air par radar doppler
GB0817570D0 (en) * 2008-09-25 2008-11-05 Secr Defence Improved weather radar
FR2945352A1 (fr) * 2009-05-05 2010-11-12 Meteo France Procede et module de determination de la vitesse d'au moins une cible par un radar meteorologique
JP2017090143A (ja) * 2015-11-06 2017-05-25 富士通テン株式会社 レーダ装置、レーダ装置用の信号処理装置及び信号処理方法
JP6500838B2 (ja) * 2016-05-18 2019-04-17 株式会社デンソー 速度検出装置
JP7168493B2 (ja) * 2018-03-23 2022-11-09 株式会社Soken レーダ装置

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Publication number Priority date Publication date Assignee Title
FR2736161B1 (fr) * 1990-12-14 1997-09-12 Le Centre Thomson D Applic Rad Procede et dispositif d'integration coherente multi-rafales pour radar doppler a impulsions
US5175551A (en) * 1991-12-18 1992-12-29 Unisys Corporation Downdraft velocity estimator for a microburst precursor detection system
US5623267A (en) * 1993-11-30 1997-04-22 Wurman; Joshua M. A. R. Wide-angle multiple-doppler radar network
DE19605568A1 (de) * 1996-02-15 1997-08-21 Daimler Benz Aerospace Ag Verfahren zur Ermittlung der Geschwindigkeit eines Radarzieles
US5808580A (en) * 1997-02-06 1998-09-15 Andrews, Jr.; Grealie A. Radar/sonar system concept for extended range-doppler coverage
DE19750742A1 (de) * 1997-11-15 1999-05-20 Daimler Benz Aerospace Ag Verfahren zur Detektion eines Zieles mittels einer HPRF-Radaranlage
JP3269441B2 (ja) * 1997-12-22 2002-03-25 三菱電機株式会社 気象レーダ装置
US6456229B2 (en) * 1999-12-13 2002-09-24 University Corporation For Atmospheric Research Bistatic radar network having incoherent transmitter operating in a scanning mode to identify scatterers
WO2001084181A2 (en) * 2000-04-24 2001-11-08 Lockheed Martin Mission Systems Passive coherent location system and method
US6710743B2 (en) * 2001-05-04 2004-03-23 Lockheed Martin Corporation System and method for central association and tracking in passive coherent location applications
FR2848675B1 (fr) * 2002-12-17 2005-05-06 Thales Sa Procede de mesure de frequence doppler par emission de trains d'impulsions lacunaires
FR2886737B1 (fr) * 2005-06-02 2007-09-07 Meteo France Etablissement Pub Procede de mesure de la vitesse de l'air par radar doppler
US7365675B2 (en) * 2005-09-26 2008-04-29 The Boeing Company Measuring wind vectors remotely using airborne radar

Non-Patent Citations (1)

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Title
See references of WO2006129006A1 *

Also Published As

Publication number Publication date
US7579977B2 (en) 2009-08-25
FR2886737B1 (fr) 2007-09-07
WO2006129006A1 (fr) 2006-12-07
FR2886737A1 (fr) 2006-12-08
US20080211714A1 (en) 2008-09-04

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