GB1239859A - Doppler radar - Google Patents

Doppler radar

Info

Publication number
GB1239859A
GB1239859A GB1556069A GB1556069A GB1239859A GB 1239859 A GB1239859 A GB 1239859A GB 1556069 A GB1556069 A GB 1556069A GB 1556069 A GB1556069 A GB 1556069A GB 1239859 A GB1239859 A GB 1239859A
Authority
GB
United Kingdom
Prior art keywords
amplitude
vehicle
output
detected
aerial
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.)
Expired
Application number
GB1556069A
Inventor
Keith Lewis Fuller
Anthony John Lambell
Derek Atter
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.)
Philips Components Ltd
Original Assignee
Mullard Ltd
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 Mullard Ltd filed Critical Mullard Ltd
Priority to GB1556069A priority Critical patent/GB1239859A/en
Publication of GB1239859A publication Critical patent/GB1239859A/en
Expired 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
    • G01S13/91Radar or analogous systems specially adapted for specific applications for traffic control
    • G01S13/92Radar or analogous systems specially adapted for specific applications for traffic control for velocity measurement
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G1/00Traffic control systems for road vehicles
    • G08G1/01Detecting movement of traffic to be counted or controlled

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

1,239,859. Doppler radar. MULLARD Ltd. 25 March, 1969, No. 15560/69. Heading H4D. Specification describes a vehicle speed detecting C.W. Doppler radar in which the speed measurement is not commenced until the vehicle has passed the radar locality and is receding at a distance determined by the amplitude of the echo signal, Fig. 3, falling to a predetermined level 7. The circuitry may be part solid state whereby the aerial (S) and said circuitry part may be assembled in a cats-eye in the middle of a traffic lane and the analysing and display means situated at a remote control point and be fed with the output of several of said cats-eye assemblies. In the embodiment of Fig. 4, an X-band Gunn-effect oscillator is amplitude modulated at 10 and the output transmitted at 13. The receiver aerial lobe is such that the amplitude of the echo signal as the vehicle nears the aerial, passes over it and then recedes, is as shown in Fig. 3. The Doppler signal produced by detector 16 is extracted by low-pass filter 17. The amplitude of the echo is detected at 27 by means of the amplitude modulation extracted at 21. Means 27 only gives an output when the amplitude is at the level 7, Fig. 3. The receding part of curve, Fig. 3, is detected by differentiator 23 and diode 26. The outputs of detector 27 and diode 26 occur simultaneously at point 8 and this event is detected at 24. An output from 24 actuates a presence counter 27 and also commences a ¢ sec. pulse from means 28. This gates the Doppler signal at 18 to the analysing and display means. The length of the vehicle may be determined by multiplying the duration of the constant (maximum) part of the amplitude curve by the vehicle's velocity.
GB1556069A 1969-03-25 1969-03-25 Doppler radar Expired GB1239859A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1556069A GB1239859A (en) 1969-03-25 1969-03-25 Doppler radar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1556069A GB1239859A (en) 1969-03-25 1969-03-25 Doppler radar

Publications (1)

Publication Number Publication Date
GB1239859A true GB1239859A (en) 1971-07-21

Family

ID=10061311

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1556069A Expired GB1239859A (en) 1969-03-25 1969-03-25 Doppler radar

Country Status (1)

Country Link
GB (1) GB1239859A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2611397A1 (en) * 1987-02-17 1988-09-02 Kone Elevator Gmbh METHOD FOR SELECTING THE OPERATING MODE OF A DEVICE USED FOR COUNTING OBJECTS IN A GIVEN AREA

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2611397A1 (en) * 1987-02-17 1988-09-02 Kone Elevator Gmbh METHOD FOR SELECTING THE OPERATING MODE OF A DEVICE USED FOR COUNTING OBJECTS IN A GIVEN AREA

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