GB1289741A - - Google Patents

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Publication number
GB1289741A
GB1289741A GB1289741DA GB1289741A GB 1289741 A GB1289741 A GB 1289741A GB 1289741D A GB1289741D A GB 1289741DA GB 1289741 A GB1289741 A GB 1289741A
Authority
GB
United Kingdom
Prior art keywords
phase shift
plane
targets
aerials
azimuth
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
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 filed Critical
Publication of GB1289741A publication Critical patent/GB1289741A/en
Expired legal-status Critical Current

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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
    • G01S13/66Radar-tracking systems; Analogous systems
    • G01S13/68Radar-tracking systems; Analogous systems for angle tracking only
    • G01S13/685Radar-tracking systems; Analogous systems for angle tracking only using simultaneous lobing techniques
    • 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
    • G01S13/42Simultaneous measurement of distance and other co-ordinates
    • G01S13/44Monopulse radar, i.e. simultaneous lobing
    • G01S13/4454Monopulse radar, i.e. simultaneous lobing phase comparisons monopulse, i.e. comparing the echo signals received by an interferometric antenna arrangement

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

1289741 Monopulse radar LICENTIA PATENT VERWALTUNGS GmbH 24 Dec 1969 [9 Jan 1969] 62915/69 Heading H4D In a phase monopulse radar, angular deviation, in two planes, e.g. azimuth and elevation, of targets from the aerial boresight is measured using five aerials, three for each plane, and for each plane combining the signals received at each aerial V 1 , V 2 , V 3 to produce the quantities (V 1 eiu1 - V 2 ), (V 2 eiu<SP>1</SP> - V 3 ) and (V 1 eiu 1 - V 2 )eiu<SP>2</SP>, where u 1 and u 2 are proportional to the azimuth or elevation angular displacements of two targets, the above quantities being used to determine u 1 and u 2 . In a first embodiment, five aerials are used in a cruciform in a plane Lr to the aerial boresight, Fig. 3. The signals received by the three aerials in the azimuth plane are given by where An = signal amplitude from target n U n = K.l.sinα n K =2#/# i α n = azimuth angle of target n l = displacement of adjacent aerials. These signals are fed to apparatus, Fig. 5, wherein V 1 undergoes a phase shift, V 2 is subtrated therefrom and the amplitude of the resultant is detected and compared with a signal derived from V 2 and V 3 in a similar manner. The above equations show that if this difference in amplitude is zero, the phase shift of V 1 and V 2 is u 1 = K.l.sinα 1 . Thus the difference signal is utilized in a feedback loop to control the two phase shift elements and the final value of phase shift determines α 1 . The equations also show that Thus the signals produced above are subtracted after the former has undergone a phase shift and the difference is fed-back to control the phase shift element. At balance the value of phase shift is u 2 =Klsinα 2 . The same procedure us used to derive the two elevation angles # 1 , # 2 . This method however gives two possible sets of co-ordinates, shown in Fig. 6 as circles and crosses respectively. In order to correlate the co-ordinates to each other, the aerial is swivelled until the boresight bisects the two azimuth angles and the two elevation angles. It is then rotated anti-clockwise about the boresight. If the elevation angles become zero first, the circles denote the targets: if the azimuth angles become zero first, the crosses denote the targets. If only one target is present, the first phase shift control voltage is zero for whatever phase shift is applied and the co-ordinates of the single target are obtained from the second phase shift elements in each plane. The same general principles are described as being applied to a system for resolving three targets (Fig. 8, not shown). In this case seven aerials are used, one extra for each plane. The correlation procedure also applies the same procedure but is much more complex. In general, to resolve v targets v + 1 aerials are used in each plane with one aerial common to both planes.
GB1289741D 1969-01-09 1969-12-24 Expired GB1289741A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691900854 DE1900854A1 (en) 1969-01-09 1969-01-09 Procedure for radar multiple target detection

Publications (1)

Publication Number Publication Date
GB1289741A true GB1289741A (en) 1972-09-20

Family

ID=5721972

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1289741D Expired GB1289741A (en) 1969-01-09 1969-12-24

Country Status (2)

Country Link
DE (1) DE1900854A1 (en)
GB (1) GB1289741A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2417118A1 (en) * 1978-02-09 1979-09-07 Siemens Ag Albis ANGULAR MEASUREMENT METHOD IN A TRACKING RADAR
GB2429860A (en) * 2005-08-31 2007-03-07 Roke Manor Research Phased array radar
CN110986947A (en) * 2019-11-29 2020-04-10 重庆交通大学 Multi-target self-propelled ship model track tracking measurement method

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
LU87671A1 (en) * 1990-01-31 1990-05-15 Ceodeux Sa TAP FOR COMPRESSED OR LIQUIFIED GAS
FR2666904B1 (en) * 1990-09-18 1993-02-12 Snecma CONTINUOUS TRANSMISSION RADAR DEVICE FOR THE SHORT-TERM DETERMINATION OF THE RELATIVE POSITION BETWEEN A MISSILE AND A TARGET MACHINE ON WHICH IT IS MOUNTED.

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2417118A1 (en) * 1978-02-09 1979-09-07 Siemens Ag Albis ANGULAR MEASUREMENT METHOD IN A TRACKING RADAR
GB2429860A (en) * 2005-08-31 2007-03-07 Roke Manor Research Phased array radar
GB2429860B (en) * 2005-08-31 2007-08-15 Roke Manor Research Phased array radar
CN110986947A (en) * 2019-11-29 2020-04-10 重庆交通大学 Multi-target self-propelled ship model track tracking measurement method
CN110986947B (en) * 2019-11-29 2023-05-02 重庆交通大学 Multi-target self-navigation ship model track tracking measurement method

Also Published As

Publication number Publication date
DE1900854A1 (en) 1970-08-13

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee