EP0479507A1 - Improvements in or relating to radar antenna arrays - Google Patents

Improvements in or relating to radar antenna arrays Download PDF

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Publication number
EP0479507A1
EP0479507A1 EP91308878A EP91308878A EP0479507A1 EP 0479507 A1 EP0479507 A1 EP 0479507A1 EP 91308878 A EP91308878 A EP 91308878A EP 91308878 A EP91308878 A EP 91308878A EP 0479507 A1 EP0479507 A1 EP 0479507A1
Authority
EP
European Patent Office
Prior art keywords
array
radar antenna
axis
along
phased array
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Withdrawn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
EP91308878A
Other languages
German (de)
French (fr)
Inventor
Peter John Wright
Christopher John Tarran
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.)
Roke Manor Research Ltd
Original Assignee
Roke Manor Research Ltd
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Filing date
Publication date
Application filed by Roke Manor Research Ltd filed Critical Roke Manor Research Ltd
Publication of EP0479507A1 publication Critical patent/EP0479507A1/en
Withdrawn legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/06Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/061Two dimensional planar arrays
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/06Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/22Antenna units of the array energised non-uniformly in amplitude or phase, e.g. tapered array or binomial array

Definitions

  • This invention relates to phased radar arrays and more especially it relates to phased planar array antennas.
  • Planar arrays normally extend in two dimensions perhaps to define a rectangular array, signals being radiated from elements of the array to form a beam which may be steered in accordance with the relative phase of the signals.
  • One of the problems associated with planar array antennas is that sidelobes of transmitted and received radar beams can be unacceptably high.
  • One known way of reducing the amplitude of sidelobes is to amplitude weight signals applied to the elements of the array.
  • Such weighting systems are well known and weighting may be applied in accordance with Hanning, Raised Cosine, or Taylor tapering functions for example.
  • This known weighting technique comprises producing an amplitude taper across the face of the array, which may be achieved by control of the amplitude of signals fed to individual elements in an active array or by using a complex network of power combiners/dividers in association with strip lines which feed power to the elements of the array.
  • Amplitude weighting as aforesaid has the disadvantage that it is inefficient since much of the power generated is lost in the weighting circuits. Moreover, the complexity of the array is significantly increased by the need for the provision of weighting circuitry in addition to the circuitry required for beam steering purposes. In a known alternative system, sidelobes are reduced by arranging the elements of the array in a non-uniform distribution ( spatial thinning).
  • a disadvantage of this kind of array is that a spatial thinning of the elements produces grating lobes at unacceptably high levels.
  • a phased array radar antenna comprises a structure which serves to support a co-ordinate array of uniformly spaced radiating elements, wherein the height of the array along one axis thereof is tapered away from the centre of the array, thereby to afford a reduction of sidelobes in a plane orthogonal to the said one axis.
  • the tapering may be arranged to be uniform about the array centre along one axis thereby to produce an array which is symmetrical about the array centre along the said one axis.
  • the element spacing may be arranged at approximately a half wavelength. This enables the formation of grating lobes to be avoided, and, since the elements of the array are each fed with power at full amplitude, without weighting, the array efficiency is not compromised.
  • the taper function used to determine the height of the array from point to point along its length and thus the effective outline of the array may be calculated in accordance with a known function such as a Hanning function, a Raised Cosine function or a Taylor function, which as hereinbefore described may be used to calculate weighting functions in known amplitude weighted systems.
  • the vertical height i.e the number of elements in each vertical column of elements is chosen to provide a required taper function across the array in accordance with the philosophy used i.e. a Hanning function, a Raised Cosine function or a Taylor function for example.
  • Figure 1 is a somewhat schematic plan view of a planar radar array comprising a plurality of elements each of which is shown.
  • a planar radar array comprises a plurality of elements 1 arranged to define in combination a coordinate array of rows and columns of elements.
  • the height of the elements in a vertical direction x is varied along the length y of the array to define a taper which extends symmetrically on each side of a centre line indicated by an arrow 2.
  • the number of the elements 1 in each column of the array may be calculated in accordance with a Hanning, or a Taylor function for example in a similar manner to the manner in which weighting coefficients would be calculated in known systems.
  • Amplitude weighting either side of the centre line 2 may be applied so that the amplitude of signals to each side of the centre line 2 is reduced whereby a reduction of sidelobes in the vertical plane is also achieved.
  • Each radiating element will be fed via an associated phase shifter and appropriate strip line networks to provide beam steering and beam formation.
  • a planar array as hereinbefore described may be embodied in one or more sides of an aircraft and thus the substrate which supports the elements of the array may form part of an aircraft superstructure.
  • the elements 1 of the array as shown in Figure 1 may comprise any known form and for example may comprise shaped radiator pads, raised studs, miniature dipoles or radiating cavities. It will also be appreciated that various modifications may be made to the arrangement hereinbefore described without departing from the scope of the invention and for example amplitude modulation in one plane may be achieved by means of attenuators, dividers or power combiners which may form a part of, or which may be included in, strip lines associated with each antenna.

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Aerials With Secondary Devices (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

A phased array radar antenna which comprises a structure which serves to support a co-ordinate array of uniformly spaced radiating elements wherein the height of the array along one axis thereof is tapered away from the centre of the array, thereby to afford a reduction of sidelobes in a plane orthogonal to the said one axis whilst retaining an efficient transmit/receiver function.

Description

  • This invention relates to phased radar arrays and more especially it relates to phased planar array antennas.
  • Planar arrays normally extend in two dimensions perhaps to define a rectangular array, signals being radiated from elements of the array to form a beam which may be steered in accordance with the relative phase of the signals.
  • One of the problems associated with planar array antennas is that sidelobes of transmitted and received radar beams can be unacceptably high. One known way of reducing the amplitude of sidelobes is to amplitude weight signals applied to the elements of the array. Such weighting systems are well known and weighting may be applied in accordance with Hanning, Raised Cosine, or Taylor tapering functions for example. This known weighting technique comprises producing an amplitude taper across the face of the array, which may be achieved by control of the amplitude of signals fed to individual elements in an active array or by using a complex network of power combiners/dividers in association with strip lines which feed power to the elements of the array.
  • Amplitude weighting as aforesaid, has the disadvantage that it is inefficient since much of the power generated is lost in the weighting circuits. Moreover, the complexity of the array is significantly increased by the need for the provision of weighting circuitry in addition to the circuitry required for beam steering purposes. In a known alternative system, sidelobes are reduced by arranging the elements of the array in a non-uniform distribution ( spatial thinning).
  • A disadvantage of this kind of array however is that a spatial thinning of the elements produces grating lobes at unacceptably high levels.
  • According to the present invention, a phased array radar antenna comprises a structure which serves to support a co-ordinate array of uniformly spaced radiating elements, wherein the height of the array along one axis thereof is tapered away from the centre of the array, thereby to afford a reduction of sidelobes in a plane orthogonal to the said one axis.
  • The tapering may be arranged to be uniform about the array centre along one axis thereby to produce an array which is symmetrical about the array centre along the said one axis.
  • In an array according to the present invention the element spacing may be arranged at approximately a half wavelength. This enables the formation of grating lobes to be avoided, and, since the elements of the array are each fed with power at full amplitude, without weighting, the array efficiency is not compromised.
  • The taper function used to determine the height of the array from point to point along its length and thus the effective outline of the array, may be calculated in accordance with a known function such as a Hanning function, a Raised Cosine function or a Taylor function, which as hereinbefore described may be used to calculate weighting functions in known amplitude weighted systems.
  • In order to achieve low sidelobes in the horizontal plane for example, the vertical height, i.e the number of elements in each vertical column of elements is chosen to provide a required taper function across the array in accordance with the philosophy used i.e. a Hanning function, a Raised Cosine function or a Taylor function for example.
  • It will be appreciated that it is practicable for a planar array only to apply a height taper function in one dimension and accordingly in order to reduce sidelobes in an orthogonal dimension, an amplitude taper may be applied in this direction using known techniques. It has been found however that since the array shape already provides a degree of tapering in this dimension the range of amplitude taper required is quite small and much less than would be required for -a conventionally shaped array and thus the efficiency reduction is correspondingly small.
  • One embodiment of the invention will now be described by way of example with reference to the accompanying drawing, in which;
  • Figure 1 is a somewhat schematic plan view of a planar radar array comprising a plurality of elements each of which is shown.
  • Referring now to Figure 1, a planar radar array comprises a plurality of elements 1 arranged to define in combination a coordinate array of rows and columns of elements. The height of the elements in a vertical direction x, as determined by the number of elements 1 in each column, is varied along the length y of the array to define a taper which extends symmetrically on each side of a centre line indicated by an arrow 2. The number of the elements 1 in each column of the array may be calculated in accordance with a Hanning, or a Taylor function for example in a similar manner to the manner in which weighting coefficients would be calculated in known systems.
  • With the arrangement shown in Figure 1, low sidelobes are achieved in a horizontal plane along the length y by tapering the height of the array in the vertical direction x.
  • Amplitude weighting either side of the centre line 2 may be applied so that the amplitude of signals to each side of the centre line 2 is reduced whereby a reduction of sidelobes in the vertical plane is also achieved. Each radiating element will be fed via an associated phase shifter and appropriate strip line networks to provide beam steering and beam formation.
  • In accordance with one embodiment of the invention a planar array as hereinbefore described may be embodied in one or more sides of an aircraft and thus the substrate which supports the elements of the array may form part of an aircraft superstructure.
  • It will be appreciated by those skilled in the art, that the elements 1 of the array as shown in Figure 1 may comprise any known form and for example may comprise shaped radiator pads, raised studs, miniature dipoles or radiating cavities. It will also be appreciated that various modifications may be made to the arrangement hereinbefore described without departing from the scope of the invention and for example amplitude modulation in one plane may be achieved by means of attenuators, dividers or power combiners which may form a part of, or which may be included in, strip lines associated with each antenna.

Claims (6)

  1. A phased array radar antenna which comprises a structure which serves to support a co-ordinate array of uniformly spaced radiating elements, wherein the height of the array along one axis thereof is tapered away from the centre of the array, thereby to afford a reduction of sidelobes in a plane orthogonal to the said one axis.
  2. A phased array radar antenna as claimed in claim 1, wherein the tapering is arranged to be uniform about the array centre along one axis thereby to produce an array which is symmetrical about the array centre along the said one axis.
  3. A phased array radar antenna as claimed in claim 1 or claim 2, wherein the element spacing is arranged to be at approximately a half wavelength.
  4. A phased array radar antenna as claimed in any preceding claim, wherein the height of the array along the said one axis thereof is determined in accordance with a Hanning or similar taper function (eg Taylor or raised cosine).
  5. A phased array radar antenna as claimed in any preceding claim, wherein an amplitude taper function is produced across the array in a direction orthogonal to the said one axis.
  6. A phased array radar antenna as claimed in any preceding claim substantially as hereinbefore described with reference to the accompanying drawing.
EP91308878A 1990-10-04 1991-09-27 Improvements in or relating to radar antenna arrays Withdrawn EP0479507A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9021638 1990-10-04
GB9021638A GB2248521A (en) 1990-10-04 1990-10-04 Radar antenna arrays

Publications (1)

Publication Number Publication Date
EP0479507A1 true EP0479507A1 (en) 1992-04-08

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Application Number Title Priority Date Filing Date
EP91308878A Withdrawn EP0479507A1 (en) 1990-10-04 1991-09-27 Improvements in or relating to radar antenna arrays

Country Status (6)

Country Link
EP (1) EP0479507A1 (en)
JP (1) JPH05503826A (en)
AU (1) AU8638091A (en)
CA (1) CA2070277A1 (en)
GB (1) GB2248521A (en)
WO (1) WO1992006519A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016071681A1 (en) * 2014-11-06 2016-05-12 Bluwireless Technology Limited Antennas
EP3255730A1 (en) * 2016-06-10 2017-12-13 Intel IP Corporation Array antenna arrangement
EP3261180A1 (en) * 2016-06-24 2017-12-27 BAE Systems PLC Aircraft radar assembly
WO2017220971A1 (en) * 2016-06-24 2017-12-28 Bae Systems Plc Aircraft radar assembly
CN112134032A (en) * 2020-09-25 2020-12-25 重庆两江卫星移动通信有限公司 Phased array antenna based on subarray arrangement and system thereof

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2324912B (en) 1994-04-18 1999-02-24 Int Mobile Satellite Org Beam-forming network
KR20040025113A (en) * 2002-09-18 2004-03-24 한국전자통신연구원 Microstrip patch array antenna for suppressing side lobes

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
IEEE 1980 INTERNATIONAL RADAR CONFERENCE April 1980, ARLINGTON,US pages 263 - 270; SMITH: 'SPACE DENSITY TAPERED ARRAYS FOR AIRBORNE SURVEILLANCE RADAR' *
IEEE TRANSACTIONS ON ANTENNAS AND PROPAGATION. vol. 30, no. 6, November 1982, NEW YORK US pages 1176 - 1183; LAXPATI: 'Planar Array Synthesis with Prescribed Pattern Nulls' *
PROCEEDINGS OF THE IEE vol. 125, no. 3, March 1978, STEVENAGE GB pages 185 - 189; F.HODJAT: 'Electronic scanning antenna using a nonuniformly-spaced planar array' *

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016071681A1 (en) * 2014-11-06 2016-05-12 Bluwireless Technology Limited Antennas
EP3255730A1 (en) * 2016-06-10 2017-12-13 Intel IP Corporation Array antenna arrangement
US20170358866A1 (en) * 2016-06-10 2017-12-14 Intel IP Corporation Array antenna arrangement
CN107634349A (en) * 2016-06-10 2018-01-26 英特尔Ip公司 Array antenna is arranged
US10637154B2 (en) 2016-06-10 2020-04-28 Intel IP Corporation Array antenna arrangement
CN107634349B (en) * 2016-06-10 2020-09-01 英特尔Ip公司 Array antenna arrangement
EP3261180A1 (en) * 2016-06-24 2017-12-27 BAE Systems PLC Aircraft radar assembly
WO2017220971A1 (en) * 2016-06-24 2017-12-28 Bae Systems Plc Aircraft radar assembly
US11067665B2 (en) 2016-06-24 2021-07-20 Bae Systems Pic Aircraft radar assembly
CN112134032A (en) * 2020-09-25 2020-12-25 重庆两江卫星移动通信有限公司 Phased array antenna based on subarray arrangement and system thereof

Also Published As

Publication number Publication date
CA2070277A1 (en) 1992-04-05
WO1992006519A1 (en) 1992-04-16
GB9021638D0 (en) 1991-04-24
AU8638091A (en) 1992-04-28
GB2248521A (en) 1992-04-08
JPH05503826A (en) 1993-06-17

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