WO2013055272A1 - Système radar à courte portée - Google Patents

Système radar à courte portée Download PDF

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Publication number
WO2013055272A1
WO2013055272A1 PCT/SE2011/051235 SE2011051235W WO2013055272A1 WO 2013055272 A1 WO2013055272 A1 WO 2013055272A1 SE 2011051235 W SE2011051235 W SE 2011051235W WO 2013055272 A1 WO2013055272 A1 WO 2013055272A1
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WO
WIPO (PCT)
Prior art keywords
antenna
transmit
receive
electronics
radar system
Prior art date
Application number
PCT/SE2011/051235
Other languages
English (en)
Inventor
Ola Forslund
Olof Eriksson
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Priority to PCT/SE2011/051235 priority Critical patent/WO2013055272A1/fr
Publication of WO2013055272A1 publication Critical patent/WO2013055272A1/fr

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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO 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
    • G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/03—Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver
    • G01S7/038—Feedthrough nulling circuits
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/32—Adaptation for use in or on road or rail vehicles
    • H01Q1/3208—Adaptation for use in or on road or rail vehicles characterised by the application wherein the antenna is used
    • H01Q1/3233—Adaptation for use in or on road or rail vehicles characterised by the application wherein the antenna is used particular used as part of a sensor or in a security system, e.g. for automotive radar, navigation systems
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/42—Housings not intimately mechanically associated with radiating elements, e.g. radome
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/06—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens
    • H01Q19/062—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using refracting or diffracting devices, e.g. lens for focusing
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/0006—Particular feeding systems
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/061—Two dimensional planar arrays
    • H01Q21/065—Patch antenna array
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00—Antenna arrays or systems
    • H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/08—Arrays of individually energised antenna units similarly polarised and spaced apart the units being spaced along or adjacent to a rectilinear path
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO 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
    • G01S13/00—Systems 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
    • G01S13/88—Radar or analogous systems specially adapted for specific applications
    • G01S13/93—Radar or analogous systems specially adapted for specific applications for anti-collision purposes
    • G01S13/931—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of land vehicles
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO 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
    • G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/027—Constructional details of housings, e.g. form, type, material or ruggedness
    • G01S7/028—Miniaturisation, e.g. surface mounted device [SMD] packaging or housings

Definitions

  • the present invention relates to a short range radar system, with microstrip patch array antennas, antenna systems and electronics arranged for wide coverage short range radar.
  • the radar solutions of today are limited to an exclusive group of users due the expensive technology required for beneficial solutions and the fact that radar installations range in size from somewhat physically voluminous for handheld or carried by a vehicle, to very large fixed installations.
  • a radar system is compiled of antennas for transmission and reception, as well as electronics. In many cases the same physical antenna is used for both transmission and reception. Some times separate antennas are required for transmission and reception.
  • the performance provided by a radar system depends on the system architecture as well as the performance figures of different parts and components in the system, and on a balance of compromises given by boundary conditions. Examples of such boundary conditions may be related to: characteristics given by a certain wavelength, distance between a transmit antenna and a receive antenna, transmission effect, signal processing accuracy, and desired product lifetime or service intervals.
  • a radar system to cover horizontally 360 degrees may require a ro- tating antenna solution.
  • Such a solution will need mechanics and service in order to operate over time. If only a limited section of the horizon is considered interesting, a fixed antenna solution with at least two separate phase coherent RF-channels in reception using so called monopulse technology could be used for determining the angular position of an object.
  • Small mechanical dimensions of a radar system are advantageous when a system is desired to harmonize with the surroundings. Small mechanical dimensions of a radar system are also advantageous, when a system is installed on a vehicle or handheld.
  • the size of the system (concerning gain, lobe widths etc) is in general inversely propor- tional to the frequency used.
  • This particular feed arrangement generates low level of stray radiation (from feed lines, power dividers, impedance transform- ers etc) and low cross polarisation for the main cuts (vertical plane and horizontal plane) due to the (anti) symmetry arrangement of the horizontal feed lines and the symmetry of the two halves.
  • this advantage only occurs for a rather small angle of interval with respect to the main cuts due to the (with respect to wavelength) large spacing between the long horizontal feed lines and the comparatively long distance between the ver- tical feed lines.
  • the length of transmission line (with respect to wavelength) per element is rather large and as a consequence the line loss per element is rather high. An antenna with these dimensions is not practical for particular applications, where small dimensions are desired.
  • US 2009/0009399 various concepts for feeding patch arrays are presented.
  • the present invention relates to a short range wide coverage radar system, in- eluding a transmit antenna and a receive antenna, both with linear polarisation.
  • An objective of the presented invention is to provide a radar system with small mechanical dimensions and with a wide H-plane coverage.
  • a radar coverage may typically be provided up to approximately 90 degrees horizontally and 15 degrees vertically, coinciding with the E-plane.
  • H-plane means the principal plane which the mag- netic field is parallel to.
  • E-plane means the principal plane which the electric field is parallel to.
  • Such a radar system may be used in surveillance applications, automotive applications, and other similar applications.
  • the invention described includes the transmit antenna, the receive antenna and electronics.
  • the electronics includes: a power distributing network to feed the transmit an- tenna, a power distributing network to feed the receive antenna, and electronics for signal processing.
  • the invention herein described presents a series fed microstrip antenna system where each sub array antenna is centrally fed via two closely spaced microstrip feed lines which are opposite in phase causing low level of stray radiation with respect to a large solid angle.
  • the length of transmission line (with respect to wavelength) per element is short, and as a consequence the line loss is low, which is advantageous in a radar system.
  • the present invention relates to conductive side-walls arranged around the transmit antenna and around the receive antenna.
  • the side walls arranged around the receive antenna widen the antenna element patterns with respect to the H-plane.
  • Conductive side-walls are advantageous when a wide coverage radar solution is desired.
  • the conductive side walls will help to widen the radar lobe of the receive antenna with respect to the H-plane.
  • Conductive side walls are also advantageous because they shield stray radiation between antennas and electronics. Without conductive side walls and the particular ra- dome arrangement the antennas would have to be positioned apart with a significant larger distance, and stray radiation would harm the performance of the radar system.
  • An embodiment includes a lens arrangement in front of the transmit antenna to widen the beam width with respect to H-plane.
  • This solution may also include a lens arrangement in front of the receive antenna.
  • a concave lens in front of the transmit antenna is advantageous to provide a wider antenna lobe.
  • a concave lens in front of the receive antenna is advantageous to provide a wider antenna lobe.
  • a preferred implementation of the antennas is by series fed microstrip patch array antennas.
  • the transmit antenna, the receive antenna and the electronics are arranged on the same printed circuit board (PCB).
  • the microstrip patch array antenna is advantageous because it can be integrated directly on a PCB.
  • Implementing a transmit antenna and a receive antenna, and electronics on the same PCB is advantageous to keep production cost low.
  • the transmit antenna is centre fed.
  • the feed to the transmit antenna may be implemented via a power splitter into two transmit microstrip lines.
  • the lengths of the two transmit microstrip lines, between the power splitter and transmit antenna differ half a guide wavelength in order for the transmit antenna to radiate in phase in a direction normal to the surface.
  • guide wavelength A g means the wavelength of the wave guided by the microstrip line.
  • the receive microstrip lines from the receive antenna are merged via a power conjunction into one feed line.
  • the lengths of the two receive microstrip lines between the power conjunction and receive antenna differ half a guide wavelength in order for the receive antenna to radiate in phase in a direction normal to the surface.
  • An advantage of having a feed line split into two/merged into one, with the lengths differing half a wavelength, and with the conjunction separated and shielded from the antenna cavity is that stray radiation originating from the feed lines is reduced and thereby side lobe levels are decreased.
  • the inner cover unit is arranged over the electronics and the power splitter.
  • the inner cover has walls joining a metal frame on the PCB.
  • the inner cover works as a shield between the antennas and the electronics.
  • the inner cover has an isolating effect on stray radiation from the electronics and the power splitter, as well as stray radiation from the antennas influencing the electronics.
  • a radome for protection of the antennas and the electronics is arranged to cover the antennas and the electronics.
  • the transmit lens and the receive lens are in an embodiment, integrated in the radome.
  • the radome is advantageously protecting the antennas and electronics from unwanted physical effect, as well as possibly carrying a desired shape and colour.
  • An advantage of integrating transmit lens and receive lens in the radome 702 is to limit the number of parts and simplify the assembly, and thereby reduce production costs.
  • Fig 1 shows a radar system 50.
  • Fig 2 shows arrays 107 and sub arrays 109.
  • Fig 3. shows transmit antenna 102 and receive antenna 104.
  • Fig 4. shows side walls 510, inner walls 512 and roof 514.
  • Fig 5A shows transmit lens 604 and receive lens 610.
  • Fig 5B. shows radar system 50 including radome 702.
  • Fig. 1 shows a radar system 50, including a PCB 100 (also referred to as printed circuit board) with a transmit antenna 102, a receive antenna 104, and electronics 106. All parts arranged on the single PCB 100.
  • the transmit antenna 102 is also referred to as microstrip patch array transmit antenna
  • the receive antenna 104 is also referred to as microstrip patch array receive antenna.
  • Fig. 1 further shows the electronics 106 connected to power splitters 1 12 and 1 13, feeding the antennas 102 and 104 via transmit microstrip lines 1 16 and receive microstrip lines 1 19.
  • the antennas 102 and 104 include patches 1 14, which are interconnected by the microstrip lines 1 16 and 1 19 respectively.
  • Fig. 2 shows the transmit antenna 102 and receive antenna 104, the antennas formed by arrays 107.
  • An array 107 may include one or a plurality of columns 108, with each column 108 divided into sub arrays 109.
  • Each sub array 109 is built by patches 1 14 fed in series, by microstrip lines 1 16 and 1 19.
  • Each sub array may be ended by a micro- strip stub 1 1 1 .
  • the transmit antenna 102 includes a centrally fed array 107, fed via one channel.
  • Two sub arrays 109 form a column 108.
  • An array may optionally comprise a plurality of columns 108.
  • Such arrangement provides a broad beam in the H- plane and a narrow in the E-plane.
  • Each sub array 109 of the centrally feed array 107 of patch elements 1 14 (patch elements may also be referred to as patches) is, according to the figure, ended by an open microstrip stub 1 1 1 .
  • Fig. 2 shows the receive antenna 104, which includes two channels, formed by two centrally fed columns 108, i.e. two columns of patches 1 14, positioned side by side.
  • the two channels signals may be superposed arbitrarily in amplitude and phase.
  • sum and difference modes in reception may be used. This is advantageous for determining a position of a target with respect to the horizontal plane, coinciding with the H-plane in the embodiment.
  • each sub array is preferably tapered, whereby the width differs slightly from individual patch to patch within each sub array in order to radiate according to a prescribed function with respect to amplitude and phase together with its op- posite half sub array 109.
  • all sub arrays 109 are substantially equal in size.
  • sub arrays 109 in an array 107 are mirrored.
  • a sampled Taylor distribution is chosen. This is one example of methods to be used for designing the array 107. Other distributions to be used for designing the array 107 include Chebyshev taper. Yet another distribution is given by that obtained when the patches are all equal in size.
  • Each sub array 109 is designed in a "travelling wave sense" meaning that, when seen as a transmitter, a time harmonic wave incident from the feed line sees a matched antenna and the wave decouples successively into free space by the patches 1 14.
  • a time harmonic wave incident from the feed line sees a matched antenna and the wave decouples successively into free space by the patches 1 14.
  • the wave has passed the last patch 1 14 virtually all energy has been decoupled into free space and only a few per cent may be left to cause reflection and stray radiation at the open microstrip stub 1 1 1. This requires that each patch 1 14 is well matched in its surrounding and the level of internal reflection is low.
  • the open microstrip stub 1 1 1 reaches effectively about one quarter of a guide wavelength from the end of the last patch 1 14 referring to the wavelength in the transmit microstrip line 1 16.
  • An alternative embodiment, not shown in Fig.2, to the open microstrip stub 1 1 1 is to end with a terminating resistor and with a quarter wave stub after the terminating resistor.
  • Yet another alternative embodiment is to short circuit the microstrip line 1 16, to the antenna ground plane of the PCB 100, immediately after the terminating resistor.
  • Such shortcut could e.g. be implemented using via holes.
  • Via holes is a term used to describe electrical connections between different layers in a PCB 100.
  • Yet another alternative embodiment is to omit the quarter wave stub and short circuit the end of the last patch in each sub array to the antenna ground plane.
  • Such shortcut could e.g. be implemented using via holes.
  • each patch 1 14 should preferably radiate a considerable amount of the incoming power.
  • An example may be for each patch 1 14 to radiate up to about 50% of the incoming power.
  • Other examples may be up to 33%, or up to 66%.
  • the patch 1 14 width has to be rather large, typically about ⁇ 0 /2 for a substrate with relative permittivity 3.66 and height 0.027 ⁇ 0 , where ⁇ 0 denotes free space wavelength. This means that unless precautions are taken the beam width in the H-plane will be considerably less than 90° which is the theoretical limit.
  • the aim is to have a wide element beam width, as close to the theoretical patch beam width with respect to H-plane as possible.
  • a thicker laminate requires a smaller patch 1 14 width and a thinner laminate requires a larger patch 1 14 width.
  • a thick laminate is not good either since it will cause more stray radiation from lines, bends and other details necessary to distribute the power in the antenna.
  • the patches 1 14 in a column 108 electrically have substantially the same distance between them. This means that the time to travel for a guided wave A g is in principal the same between each patch 14.
  • the patches 1 14 in a column 108 have substantially the same physical distance between them.
  • the transmit antenna 102 and the receive antenna 104 are ar- ranged side by side, with columns 108 parallel to each other, as shown in Fig 2. And the arrays 107 of patches 1 14 are thus vertically polarised.
  • the E-plane thus coincides with the vertical plane and the H-plane with the horizontal in this case. This is advantageous because it will provide a considerably better isolation between transmit antenna 102 and receive antenna 104, in comparison to if they were arranged side by side and fed as to be horizontally polarized. A large signal isolation between the transmit antenna 102 and re- ceive antenna 104, is desired.
  • the transmit antenna 102 and the receive antenna 104 are arranged vertically in line with each other.
  • the transmit antenna 102 and the receive antenna 104 are arranged horizontally in line with each other.
  • the polarisation will be horizontal in this case.
  • the arrangement in Fig. 2 is rotated 90 degrees, so that the arrays are still arranged in parallel but with one now on top of the other.
  • the polarisation will be horizontal in this case.
  • Fig. 3 shows a transmit antenna 102 and a receive antenna 104, including arrays 107 and sub arrays 109.
  • Electronics 106 feed power splitters 1 12 and 1 13 via feed lines 1 17 and 1 18.
  • the power splitters 1 12 and 1 13 feed the antennas, via microstrip lines 1 16 and 1 19.
  • Further Fig. 3 shows metal frames 408 arranged around the antennas 102 and 104.
  • each sub array 109 in the arrays 107 include a central feed via two separate parallel, with respect to ⁇ 0 , rather closely spaced, transmit microstrip lines 1 16 and 1 19, con- nected to a common power splitter 1 12 and 1 13.
  • the distance between the parallel feed lines is around ⁇ 0 /10, which is considered closely spaced with respect to ⁇ 0 .
  • the lengths of the two transmit microstrip lines 1 16 and 1 19 differ half a guide wavelength seen from the power splitters 1 12 and 1 13 to the antennas 102 and 104, in order for the sub arrays 109 of the arrays 107 to radiate in phase in a direction normal to the PCB.
  • the feed lines 1 17 and 1 18 may have a lower impedance on the electronics 106 side of the power splitter 1 12, than the microstrip lines 1 16 and 1 19 on the antennas 102 and 104 sides of the power splitters 1 12 and 1 13.
  • the feed line 1 17 and 1 18 on the electronics 106 side may have 50 Ohm.
  • microstrip lines 1 16 and 1 19 on the on the antennas 102 and 104 side may have 80 Ohm, with the appropriate impedance transformer integrated in the power splitter 1 12 and 1 13.
  • the appropriate impedance transformer integrated in the power splitter 1 12 and 1 13.
  • the impedance values on both sides of the power splitter 1 12 and the junction 1 13 should only be seen as examples. It should be understood that other values may be selected depending on preferred system impedance, permittivity, and height of PCB substrate.
  • 1 19 is ⁇ /4, or ⁇ 0 /20, or a value between ⁇ 0 /4 and ⁇ 0 /20.
  • the distance between a ground plane in the PCB 100 and the transmit microstrip lines 1 16 is shorter, than the distance between the two parallel transmit microstrip lines 1 16. And the distance between a ground plane in the PCB 100 and the re- ceive microstrip lines 1 19 is shorter, than the distance between the two parallel receive microstrip lines 1 19.
  • the power splitters 1 12 and 1 13 are located outside the antenna 102 and 104 cavities and may be surrounded by shielding and lossy side walls 510 and roof 514 (further described in Fig.4) as the rest of the electronics 106.
  • Beneath the side walls 510 metal frames 408 are arranged on the PCB 100.
  • Metal frames 408 are surrounding the transmit antenna 102 and the receive antenna 104.
  • the sidewalls 510 and metal frames 408 are physically and electrically connected in such a way that together they form walls around the antennas 102 and 104.
  • the walls enclose the antennas 102 and 104, and the walls and the roof 514 together enclose the electronics 106.
  • the metal frames 408 may be implemented by a metal foil and closely spaced metallic posts, e.g. via holes, which also are connecting the metal foil formed around the antennas (102, 104), with the ground plane (not shown in Figures). Via holes are advantageously closely spaced together relative to the wavelength, in order to shield radiation.
  • the term "power splitter” 1 12 may be used both for the function to split the feed from electronics 106 to the transmit antenna 102, as well as the function to merge the feeds from the receive antenna 104 to the electronics 106. Another term for the power splitter located between the receive antenna 104 and the electronics 106, is junction 1 13.
  • the receive antenna 104 includes two columns. It is possible to show that the stray radiation for a 2D, two dimensional, case is reduced by a factor 0(a/p) for the two parallel microstrip line feed solution where "a” is the distance between the parallel lines, "p” is the orthogonal distance to the field point and “O” is the "large ordo symbol” used in mathematics .
  • the two centrally fed sub arrays 109 of patches may be closely spaced.
  • the power splitter 1 12 and 1 13 may be located outside the transmit antenna 102 cavity and isolated in order not to receive or contribute with stray radiation.
  • Fig. 4 shows the PCB 100, already described, for a radar system 50 with the antennas 102 and 104 surrounded by metal frames 408.
  • Fig. 4 also shows inner cover 516, including side walls 510, inner walls 512, roof 514 and cavities 518 for power splitters 1 12 and 1 13, from a perspective view.
  • Side walls 510, inner walls 512 and roof 514 may collectively be described as inner cover 516.
  • the side walls 510, inner walls 512 and roof 514 is formed in one single unit.
  • the inner cover 516 is also described as conductive covering 516.
  • the PCB 100 is shown with the antennas facing upwards, and the inner cover 516 is shown with the inside facing upwards.
  • metal frames 408 and inner cover 516 complete structures, is not shown.
  • metal frames 408 and inner cover 516 shown in Fig. 4 surrounding power splitter 1 12 and 1 13, is not shown in Fig. 3 because it would make Fig 3 difficult to read.
  • the power splitter 1 12 and junctions 1 13 are each located in separate cavities 518 formed by the PCB 100 and the inner walls 512 and the roof 514.
  • the transmit antenna 102 and the receive antenna 104 are enclosed by side walls 510.
  • the side walls 510 may shield the electronics 106 from stray radiation of the antennas.
  • the side walls 510 are both electrically conductive and provide attenuation of electromagnetic waves.
  • materials which can provide such characteristics including: metals, plastics, or combinations thereof.
  • An optimal balance is desired of electrical conductivity which shield electromagnetic waves, and attenuation which absorb the electromagnetic waves.
  • the inner cover 516 may comprise metalized plastic fibres, with a coal suspension added to it.
  • Fig. 4 shows vertically oriented conducting side walls 510 placed adjacent to the patch array.
  • the side walls 510 parallel with columns 108, form a so called parallel plate waveguide.
  • the parallel plate waveguide transforms the radiating aperture and phase centre away from the patches 1 14 surface to the waveguide aperture.
  • a sinus shaped field taper will be created with respect to the horizontal direction, coinciding with the H-plane. This will happen provided the side walls 510 on the long side are high enough giving the possibility of a beam wide enough for a particular application.
  • the side walls 510 may in an embodiment be arranged separately around the antennas 102 and 104, and thereby provide the described advantageous features.
  • Fig. 5A shows a PCB 100 seen from the side, comprising a transmit antenna 102, a receive antenna 104.
  • Fig. 5A also shows a transmit lens 604 and a receive lens 610.
  • the transmit lens 604 is arranged on top of the transmit antenna 102, with the PCB 100 surface upwards. I.e. radiation transmitted from the patches 1 14 is radiated through the transmit lens 604, on the way from the transmit antenna 102. According to the figure, the transmit lens 604 widens the transmit antenna 102 beam with respect to the H-plane. By arrangement of the transmit lens 604 in front of the transmit antenna 102, the antenna beam is refracted to a wider beam. This is advantageous for a short range wide coverage radar system 50.
  • each column of the receive antenna 104 has its own re- ceive lens 610, which individually widens the pattern of its corresponding column with respect to the H-plane.
  • the receive lens 610 is arranged on top of the receive antenna 104, with the PCB 100 surface upwards. I.e. radiation received to the patches 1 14 is passed through the receive lens 610, on the way to the receive antenna 104.
  • the receive lens 610 widens the receive antenna 104 beam with respect to each column in the H-plane.
  • the antenna beam corresponding to each column is refracted to a wider beam with respect to H-plane. This is advantageous because a receive antenna 104 can then operate in a wide coverage radar system 50.
  • the transmit lens 604 and the receive lens 610 may be shaped as concave cylindrical lenses.
  • the transmit lens 604 is arranged to broaden the transmit antenna 102 radiation pattern with respect to the H-plane.
  • the H-plane coincides with the horizontal plane in this case, which is advantageous for a wide coverage short range radar system 50.
  • the energy flow is virtually orthogonal to the aperture, in this solution the patches 1 14 surface.
  • the transmit lens 604 may refract the rays in such a way that the energy seems to emanate from a point above the surface of the patches 1 14.
  • the transmit lens 604 may thereby move the phase centre of each sub array away from the patches 1 14 surface in the direction of the beam.
  • the beam may be widened. A wide beam is desired, and thereby advantageous for a short rage wide coverage radar system 50.
  • the receive lens 610 may widen the radiation pattern received by each column of the receive antenna 104 with respect to the H-plane. Thereby the received beam may be widened in the H-plane with respect to each column.
  • the H-plane coincides with the horizontal plane in this case, which is advantageous for a wide coverage short range radar system 50.
  • the energy flow is virtually orthogonal to the aperture, in this solution the patches 1 14 surface.
  • the receive lens 610 may refract the rays in such a way that the energy seems to emanate from a point above the surface of the patches 1 14.
  • the receive lens 610 may thereby move the phase centre of each sub array 109 away from the patches 1 14 surface in the direction of the beam. Moreover the beam may be widened.
  • a wide received beam for each column 108 is desired, and thereby advantageous for a short rage wide coverage radar system 50.
  • Fig. 5B shows a radar system 50, including the inner cover 516 shown in Fig. 4.
  • PCB 100 with transmit antenna 102 and receive antenna 104, previously shown.
  • radome 702 with transmit lens 604 and receive lens 610. The different parts in Fig. 5B, are shown with some distance apart.
  • the radome 702 is arranged for its normal purpose, to cover the antennas and the electronics.
  • the transmit lens and the receive lens are in an embodiment, integrated in the radome 702.
  • radome 702 An advantage of the radome 702 is to protect the antennas and electronics from unwanted physical effect, as well as possibly carrying a desired shape and colour.
  • radome 702, the transmit lens 604, and the receive lens 610 are separate units, but essentially providing the same functionality as above.
  • a combination utilizes beam widening by the transmit lens 604, and the receive lens 610, and beam widening by the conducting side walls 510 creating parallel plate waveguide modes.
  • the conducting side walls 510, transmit lens 604 and receive lens 610 may well be used separately, but used together they will cooperate for a better effect of a wide antenna beam with respect to the H- plane for each column.
  • this combination effect of side walls 510 and the receive lens 610 is only utilized in the receive antenna 104, while the transmit antenna 102 obtains beam widening only by the transmit lens 604.
  • the combination of side walls 510 and lens 604 is only utilized in the transmit antenna.
  • such a system typically has a coverage with respect to the horizontal plane with some 90° and with coverage of approximately 15° in elevation. Examples of other typical coverage's are; horizontal plane with some 45° and some 7° in elevation.
  • the distance between the transmit antenna 102 and the receive antenna 104 is maximum 10 cm, or 50 cm.
  • the radar system 50 is operating on a frequency around 10
  • GHz or 24 GHz, or 77 GHz, or in a range from 10 GHz to 77 GHz.
  • the radar system 50 is operating in a range of 0 to 200 meter, or 0 to 400 meter, or 0 to 800 meter.

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

Abstract

La présente invention a trait à une carte de circuit imprimé (100) destinée à un système radar (50) pour la détection à courte portée d'objets, laquelle carte de circuit imprimé comprend une antenne d'émission réseau de correction à microruban (102) qui est agencée de manière à transmettre un rayonnement, une antenne de réception réseau de correction à microruban (104) qui est agencée de manière à recevoir un rayonnement et de l'électronique (106) destinée au radar et au traitement des signaux, laquelle électronique (106) est agencée de manière à alimenter l'antenne d'émission (102), à alimenter à partir de l'antenne de réception (104) et à traiter les signaux. Ladite carte de circuit imprimé (100) comprend un cadre métallique (408) qui est agencé autour de l'antenne d'émission (102) afin d'assurer l'isolation entre l'antenne d'émission (102), l'antenne de réception (104) et l'électronique (106) ; la carte de circuit imprimé (100) comprend aussi un cadre métallique (408) qui est agencé autour de l'antenne de réception (104) afin d'assurer l'isolation entre l'antenne d'émission (102), l'antenne de réception (104) et l'électronique (106). La présente invention a également trait à un système radar (50) permettant de détecter à courte portée des objets, lequel système radar comprend une carte de circuit imprimé (100) ainsi que des parois latérales conductrices (510) qui sont agencées autour de l'antenne d'émission (102) coopérant avec le cadre métallique (408), afin d'assurer l'isolation entre l'antenne d'émission (102), l'antenne de réception (104) et l'électronique (106) ; le système radar (50) comprend également des parois latérales conductrices (510) qui sont agencées autour de l'antenne de réception (104) coopérant avec le cadre métallique (408), afin d'assurer l'isolation entre l'antenne d'émission (102), l'antenne de réception (104) et l'électronique (106).
PCT/SE2011/051235 2011-10-14 2011-10-14 Système radar à courte portée WO2013055272A1 (fr)

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US9332680B2 (en) 2013-03-15 2016-05-03 Autoliv Asp, Inc. Electrical gasket and electronic module having electrical gasket
WO2017153073A1 (fr) * 2016-03-11 2017-09-14 Robert Bosch Gmbh Dispositif antenne pour détecteur radar
CN107437660A (zh) * 2017-08-15 2017-12-05 湖南华诺星空电子技术有限公司 一种步进频连续波穿墙雷达的天线装置
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WO2018072826A1 (fr) * 2016-10-20 2018-04-26 G. Lufft Mess- Und Regeltechnik Gmbh Dispositif et procédé de mesure de précipitations
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WO2019026638A1 (fr) * 2017-07-31 2019-02-07 ダイキン工業株式会社 Unité de capteur et climatiseur
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WO2022271646A1 (fr) * 2021-06-24 2022-12-29 ForSight Technologies Inc. Capteurs térahertz et systèmes et procédés associés

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US9332680B2 (en) 2013-03-15 2016-05-03 Autoliv Asp, Inc. Electrical gasket and electronic module having electrical gasket
WO2017153073A1 (fr) * 2016-03-11 2017-09-14 Robert Bosch Gmbh Dispositif antenne pour détecteur radar
US10996330B2 (en) 2016-03-11 2021-05-04 Robert Bosch Gmbh Antenna device for a radar sensor
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CN110945375A (zh) * 2017-07-31 2020-03-31 大金工业株式会社 传感器单元和空调机
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CN107611577A (zh) * 2017-09-06 2018-01-19 上海通趣科技有限公司 一种基于77GHz毫米波雷达的微带阵列天线
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CN109638437A (zh) * 2018-12-07 2019-04-16 长沙瑞感电子科技有限公司 一种mimo毫米波微带阵列天线
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CN109768372A (zh) * 2019-02-22 2019-05-17 苏州闻颂智能科技有限公司 一种应用于毫米波雷达的串并结合馈电微带阵列天线
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CN112787076A (zh) * 2019-11-06 2021-05-11 华为技术有限公司 天线结构、雷达和终端
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WO2022021430A1 (fr) * 2020-07-31 2022-02-03 深圳市大疆创新科技有限公司 Réseau d'antennes, radar et plateforme mobile
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CN112599961A (zh) * 2020-12-02 2021-04-02 惠州Tcl移动通信有限公司 一种天线结构及电子设备
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