CN109444891A - A kind of millimetre-wave radar antenna system and decoupling method - Google Patents

A kind of millimetre-wave radar antenna system and decoupling method Download PDF

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Publication number
CN109444891A
CN109444891A CN201910014117.8A CN201910014117A CN109444891A CN 109444891 A CN109444891 A CN 109444891A CN 201910014117 A CN201910014117 A CN 201910014117A CN 109444891 A CN109444891 A CN 109444891A
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antenna
receiving antenna
receiving
millimetre
transmitting
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陈启生
其他发明人请求不公开姓名
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Zhejiang Libang Hexin Intelligent Brake System Co Ltd
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Zhejiang Libang Hexin Intelligent Brake System Co Ltd
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    • 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
    • G01S13/93Radar or analogous systems specially adapted for specific applications for anti-collision purposes
    • G01S13/931Radar or analogous systems specially adapted for specific applications for anti-collision purposes of land vehicles
    • 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
    • G01S7/03Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver

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  • 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)

Abstract

The invention discloses a kind of millimetre-wave radar antenna system and decoupling methods, the antenna system includes aerial array, primary processor and baseband processing circuitry, the aerial array includes at least 2 transmitting antennas and at least 2 receiving antennas, the transmitting signal of primary processor is radiated to object by transmitting antenna, receiving antenna receives target echo, signal obtains each target component after primary processor is mixed to base band, by baseband processing circuitry analytical calculation.Compared with equal performance radar, the antenna system is using single processing integrated chip scheme, and cost is relatively low, and mainboard and antenna element are more compact.Using the decoupling method, target bearing and pitch angle can be calculated, and by the equivalent virtual array principle of MIMO, above-mentioned antenna system can fictionalize more receiving channels, improve azimuth determination resolution ratio.It using the monopulse antenna structure in the antenna system, can solve when receiving antenna interval is larger, main beam shapes the fuzzy problem of azimuth angle measurement.

Description

A kind of millimetre-wave radar antenna system and decoupling method
Technical field
The present invention relates to a kind of antenna system and decoupling method, in particular to a kind of millimetre-wave radar antenna system and decoupling Method.
Background technique
Vehicle-mounted millimeter wave radar has become major vapour as a kind of active prevention apparatus for improving automotive safety coefficient The emphasis of depot quotient and the majority of consumers' concern.Radar by the reflection signal of processing target object thus obtain the distance of object, The information such as speed, angle.Cardinal principle is to generate a specific waveform first inside radar, wherein the beam signal of fraction It is used as reference signal, and in addition most beam signal is gone out by aerial radiation.The signal being radiated is being propagated through It encounters target in journey then to reflect, reflected signal is received antenna and receives and be mixed with reference signal, radar Baseband circuit on plate can be handled this mixed frequency signal, obtain the relative velocity of Ben Che and other objects, azimuth, The information such as distance.System judges these information, when system identification is dangerous, can be slowed down automatically, be braked, with This protection ride safety of automobile.In vehicle travel process, for the trailer-mounted radar of no pitching angle measurement ability, can by some for Driving safety is almost without in the traffic related compounds (such as pop can in road center, inspection well cover etc.) and normally travel road of influence Tunnel, bridge opening etc., be considered as risk object, to take emergency braking measure, seriously affect driving experience and driver's life Safety;Therefore, for vehicle-mounted millimeter wave radar in addition to azimuth determination, pitch angle angle measurement ability is also extremely important.
Currently, millimetre-wave radar antenna mainly in the form of micro-strip paster antenna based on, mostly use multiple-input multiple-output (MIMO) greatly System, and multiple-input multiple-output system generate equivalent more receiving channels Signal-to-Noise although can be improved, to improve ranging Angle measurement accuracy, but may have following deficiency:
1, when the interval between millimetre-wave radar adjacent reception antenna is larger, there are angle measurements to obscure for main beam forming results, When being greater than 0.5 λ such as the interval between millimetre-wave radar adjacent reception antenna, radar bearing angle measurable angle range [- αminmax] be less than 90 degree, when azimuth of target α is not within the scope of radar angle measurement, azimuth of target can be mapped as one within the scope of radar angle measurement Angle [alpha]m, so that radar receiving end can not judge that the actual value of the angle is α or αm, i.e., there are ambiguities for angle measurement result Problem;
2, in order to realize higher resolution ratio, integrated using multi-chip, cost is very high, and radar volume is also more huge;
3, when three traditional four acceptor systems of hair have pitch angle and azimuth determination function at the same time, the reception fictionalized is logical Road is often less, causes azimuth resolution lower.
In view of this, the present inventor studies this, a kind of millimetre-wave radar antenna system and decoupling are specially developed Thus method, this case generate.
Summary of the invention
The object of the present invention is to provide a kind of millimetre-wave radar antenna system and decoupling methods.
To achieve the goals above, solution of the invention is:
A kind of millimetre-wave radar antenna system, including aerial array, primary processor and baseband processing circuitry, the antenna array Column include at least 2 transmitting antennas, and at least 2 receiving antennas, and the transmitting signal of primary processor is radiated by transmitting antenna To object, receiving antenna is received by the reflected signal of object, and the signal is after primary processor is mixed, by base band Processing circuit analytical calculation obtains each target component.
Preferably, every transmitting antenna includes at least one linear array;The every receiving antenna includes at least one A linear array.
Preferably, the linear array includes several patches, the patch is the patch that width is weighted.By to every The width of a patch is weighted, and changes the current strength of each patch, is then changed the overall current distribution of linear array, is reduced secondary Valve, weighting scheme are distributed using Chebyshev, realize that the equal minor lobes of wave beam are distributed.
Preferably, the aerial array includes 3 transmitting antennas and 4 receiving antennas.
Preferably, the aerial array includes the first transmitting antenna set gradually, the second transmitting antenna, the first reception Antenna, the second receiving antenna, third receiving antenna, the 4th receiving antenna and third transmitting antenna;Wherein, the first receiving antenna away from It is d from the lateral separation at the second receiving antenna and third receiving antenna centerx3, wherein 3 λ≤dx3≤4.5λ;Second receives day Lateral separation d between line, third receiving antennax4=0.5 λ, the 4th the second receiving antenna of receiving antenna distance and third receive The lateral separation d of center of antennax5=dx3, lateral separation d between first transmitting antenna, the second transmitting antennax1=dx3/ 2, longitudinal gap dy1=1.4 λ, the lateral separation d between the second transmitting antenna and third transmitting antennax2=3dx3, longitudinal gap It is 0;Wherein the λ is carrier wavelength.
A kind of millimetre-wave radar antenna decoupling method, includes the following steps:
1) each transmitting antenna in aerial array emits signal simultaneously, with phase, and signal is after object reflects, by each Receiving antenna receives;
2) equivalent virtually to obtain the virtual antenna arrays being made of N receiving antenna according to the equivalent virtual array principle of MIMO Column, N are the product of practical receiving antenna quantity and number of transmission antennas;
3) phase value at each receiving antenna center in virtual antenna array is calculated according to formula (1):
Wherein n=1,2,3 ... N, dazFor the horizontal spacing between each receiving antenna of virtual antenna array, delFor virtual day Longitudinal pitch between each receiving antenna of linear array, λ are carrier wavelength, and θ is azimuth of target, and φ is pitch angle, are obtained virtual Total phase set of receiving antenna in aerial array
4) each phase value in total phase set is arranged to by several subsets, the subset packet according to function difference Include main beam collectionFirst wavelet constrictionSecond wavelet constrictionWith pulse collectionIn wherein one or more;
5) to the main beam collectionPower estimation calculation is carried out, azimuth of target θ is obtained1;To the first beamletCollection carries out Power estimation is calculated, and pitch angle φ is obtained;To the second wavelet constrictionPower estimation calculation is carried out, azimuth of target θ is obtained2, to the list Pulse setUsing than phase algorithm, obtain without fuzzy azimuth.
Preferably, the main beam collection
Preferably, the first wavelet constrictionIncluding total phase setEach phase value of middle front half, i.e.,
Preferably, the second wavelet constrictionIncluding total phase setEach phase value when middle n is even number, i.e.,
Preferably, the pulse collectionIncluding being divided into each phase corresponding to the virtual receiving antenna of 0.5 λ between two Place value.
Millimetre-wave radar antenna system of the present invention, using single master chip processor, cost is relatively low, is suitble to big rule Modulus produces;It is compared simultaneously with equal performance radar, antenna element of the present invention is more compact, and dual-mode antenna is less, radar Occupied space is smaller, helps to be mounted on narrow vehicle interior.Using the millimetre-wave radar antenna system of above-mentioned decoupling method, Azimuth and the pitch angle of measurement target can be calculated, when receiving antenna interval is larger, carried out using 2 sub- beam formings Angle measurement solves the problems, such as that main beam shapes angle measurement ambiguity;Moreover, have pitch angle, azimuth determination function it is same When, more receiving channels can be fictionalized, azimuth determination resolution ratio is further increased.
Below in conjunction with drawings and the specific embodiments, the invention will be described in further detail.
Detailed description of the invention
Fig. 1 is the millimetre-wave radar antenna system working principle diagram of the present embodiment;
Fig. 2 is the layout of the aerial array of the present embodiment;
Fig. 3 is the layout of the virtual antenna array of the present embodiment.
Specific embodiment
Millimetre-wave radar antenna system 2 described in the present embodiment, mountable front or side in vehicle 1, such as Fig. 1 institute Show, the millimetre-wave radar antenna system 2 includes 3, primary processors 4 of aerial array and a Base-Band Processing of multiple-input multiple-output Circuit 5, the present embodiment are described in detail with the aerial array that three hairs four are received.The aerial array 3 includes the be arranged successively One transmitting antenna TX1, the second transmitting antenna TX2, the first receiving antenna RX1, the second receiving antenna RX2, third receiving antenna RX3, the 4th receiving antenna RX4 and third transmitting antenna TX3.Each transmitting antenna and receiving antenna are micro-strip antenna array, work Frequency is located at car radar regulation use scope (76~81GHz).
In the present embodiment, the first transmitting antenna TX1, the second transmitting antenna TX2, third transmitting antenna TX3 are One linear array, can also be using the transmitting antenna of two linear arrays or three linear arrays.When there are 2 or more linear arrays, need diligent Device is divided to be attached.The first receiving antenna RX1 and the 4th receiving antenna RX4 structure are identical, include power splitter, and string Two linear arrays being associated on power splitter, the second receiving antenna RX2, third receiving antenna RX3 structure are identical, using a line Battle array, wave beam is wider, and gain relative transmission antenna is more lower.It is connected between the two adjacent linear array on the same power splitter Between be divided into 0.5 λ, the λ is carrier wavelength (i.e. operation wavelength), such as the free space wavelength at centre frequency 76.5GHz.
As shown in Fig. 2, lateral separation refers to interval along the x axis in X-Y coordinate, longitudinal gap refers to along Y-axis The interval in direction, the lateral separation d between the first transmitting antenna TX1 and the second transmitting antenna TX2x1=1.5 λ, between longitudinal direction Every dy1=1.4 λ, the lateral separation d between the second transmitting antenna TX2 and third transmitting antenna TX3x2=9 λ, longitudinal gap 0 (that is, in same level);First receiving antenna RX1 distance the second receiving antenna RX2 and the center third receiving antenna RX3 Lateral separation is dx3=3 λ, the lateral separation between the second receiving antenna RX2, third receiving antenna RX3 are dx4=0.5 λ, the The lateral separation at four receiving antenna RX4 distance the second receiving antenna RX2 and the center third receiving antenna RX3 is dx5=3 λ, first Receiving antenna RX1, the second receiving antenna RX2, third receiving antenna RX3, the 4th receiving antenna RX4 longitudinal gap be 0 (that is, In same level);The longitudinal gap of described second transmitting antenna TX2 (or third transmitting antenna TX3) and each receiving antenna For dy2, dy2Value can rationally be adjusted according to radar laying out pattern, do not influence calculated result.
The linear array of each transmitting antenna and receiving antenna includes 10 patches in the present embodiment, and the patch is width by adding The patch of power, reduces minor lobe by the way of amplitude weighting along the y-axis direction.It is weighted by the width to each patch, Change the current distribution of each patch, reduce minor lobe, weighting scheme is distributed using Chebyshev, realizes that the equal minor lobes of wave beam divide Cloth.
General transmitting antenna patch is some more, and gain is larger, can be used for improving target detection range.And receiving antenna patch Less, wave beam is wider, can be used for expanding target detection angle.In actual use, some does not need to test too far Distance, and some need extension detection angles etc., can be depending on radar actual test demand.
The first transmitting antenna TX1, the second transmitting antenna TX2, third transmitting antenna of above-mentioned millimetre-wave radar antenna system 2 TX3 simultaneously goes out the signal radiation of primary processor 4, and electromagnetic wave encounters object 6 during spatial and by object 6 It is reflected back the first receiving antenna RX1, the second receiving antenna RX2, third receiving antenna RX3, the 4th for being arranged on different location Receiving antenna RX4, then this high-frequency signal is mixed by primary processor 4 with local oscillation signal, is transmitted in baseband circuit 5 and is carried out Processing, because having certain interval between adjacent 2 receiving antennas, this, which will lead to the signal that every receiving antenna receives, has Certain phase difference.By handling this phase difference, multiple angle informations of object 6 can be obtained.
Three four acceptor millimetre-wave radar antenna systems of hair described in the present embodiment, using single master chip processor, at This is lower, is suitble to scale of mass production;It is compared simultaneously with equal performance radar, antenna element of the present invention is more compact, receives Hair antenna is less, and radar occupied space is smaller, helps to be mounted on narrow vehicle interior.
The decoupling method of millimetre-wave radar antenna system based on four acceptors of above-mentioned three hair, includes the following steps:
1) the first transmitting antenna TX1 in aerial array, the second transmitting antenna TX2, third transmitting antenna TX3 be simultaneously, together Mutually transmitting signal, the signal launched is after the reflection of object 6, by the first receiving antenna RX1, the second receiving antenna RX2, third Receiving antenna RX3, the 4th receiving antenna RX4 are received.
2) according to the equivalent virtual array principle of MIMO, it is equivalent virtually obtain being made of 12 (3*4) receiving antennas it is virtual Aerial array, as shown in figure 3, its equivalent virtual receiving antenna array can indicate are as follows: { RX1, RX2, RX3+RX4, RX5+ RX6, RX7, RX8,0, RX9,0, RX10+RX11,0, RX12 }
Total phase set of corresponding virtual receiving antenna array are as follows:
3) phase value at each receiving antenna center in virtual antenna array is calculated according to formula (1):
Wherein n=1,2,3,4L 12, dazFor the horizontal spacing between each receiving antenna of virtual antenna array, delIt is virtual Longitudinal pitch between each receiving antenna of aerial array, in the present embodiment, preferably daz=1.5 λ, del=1.4 λ, λ are carrier wave Wavelength, θ are azimuth of target, and φ is pitch angle.
4) each phase value in total phase set of the virtual receiving antenna is arranged to by several according to function difference Subset, each subset are respectively used to calculate different parameters, the quantity of subset according to actual needs depending on, in the present embodiment, The subset includes main beam collection(Main-beamformer), the first wavelet constriction(Sub-beamformer1), second Wavelet constriction(Sub-beamformer2) and pulse collection(Monopulse), wherein the main beam collectionIncluding total Phase setIn all phase values, i.e.,The first wavelet constrictionIncluding Total phase setIn before half phase value, i.e.,The second wavelet constriction Including total phase setEach phase value when middle n is even number, i.e.,The pulse CollectionIncluding being divided into each phase value corresponding to the virtual receiving antenna of 0.5 λ between two, i.e.,
5) to the main beam collectionEstimate to obtain frequency corresponding to azimuth of target using maximum- likelihood estimation, To which estimation obtains azimuth angle theta1.Maximum- likelihood estimation calculation amount is larger, and the common algorithm that simplifies is Fourier transformation, obtains The result obtained is the approximation of maximum likelihood algorithm result.In addition, super resolution algorithm such as MUSIC algorithm, ESPIRIT algorithm etc. because It is widely used in angle estimation with higher angular resolution.By main beam collectionThe azimuth of target θ being calculated1, Because of main beam collectionThe phase that FFT is participated in forming is most, and the accumulation gain of target bearing is maximum, thus has maximum noise Than;Target bearing resolution capability under single goal scene is best;It is preferable for the multi-sources distinguishing ability with similar orientation angle;
6) to the first wavelet constrictionEstimate to obtain corresponding to target pitch angle using maximum- likelihood estimation Frequency, so that estimation obtains pitch angle φ.Maximum- likelihood estimation calculation amount is larger, and the common algorithm that simplifies is Fourier's change It changes, the result of acquisition is the approximation of maximum likelihood algorithm result.Fourier transformation obtain Liang Ge local peaking, the part The ratio between peak value has specific mathematical relationship with pitch angle, calculates pitch angle according to this mathematical relationship.In addition, super resolution algorithm is such as MUSIC algorithm, ESPIRIT algorithm etc. are widely used in pitch angle estimation due to higher angular resolution.
7) to the second wavelet constrictionEstimate to obtain corresponding to azimuth of target using maximum- likelihood estimation Frequency, so that estimation obtains azimuth angle theta2.Maximum- likelihood estimation calculation amount is larger, and the common algorithm that simplifies is Fourier's change It changes, the result of acquisition is the approximation of maximum likelihood algorithm result.In addition, super resolution algorithm such as MUSIC algorithm, ESPIRIT is calculated Method etc. is widely used in orientation angles estimation due to higher angular resolution.Because the second wavelet beam shaping is not by pitching Angle information influences, can accurate estimation orientation angle information.And azimuth angle measurement accuracy phase of the result under multiple target scene To best, and there is relatively good multi-sources distinguishing ability.But, since the second beam subset antenna spacing is greater than λ/2, thunder Up to azimuth measurable angle range [- αminmax] less than 90 degree, when azimuth of target α is not within the scope of radar angle measurement, target bearing Angle can be mapped as an angle [alpha] within the scope of radar angle measurementm, so that radar receiving end can not judge the actual value of the angle It is α or αm, i.e., there are angle measurements to obscure for angle measurement result, for example, when being divided into 3 λ/2 between the second beamlet concentration respective antenna, angle measurement Range is positive and negative 19.5 degree, then the azimuth spent for 41.8 degree or -41.8 can all be mapped as 0 degree, so working as radar receiving end When measuring 0 degree of angle, can not judge it is 0 degree, it is fuzzy to have angle measurement for 41.8 degree of still -41.8 degree.
8) for the pulse collectionUsing than phase algorithm, obscured to solve angle measurement.Specifically,Three of set Phase valueThree groups of Monopulse estimation structures are respectively corresponded, every group of angle measurement structure is by being divided into λ/2 between two Antenna is constituted, and measurable angle range is positive and negative 90 degree.The phase difference that target echo causes two antennas certain, using can than phase algorithm To obtain azimuth of target, to the azimuth of target weighted sum that three groups of phase values calculate separately, for improving angle measurement letter It makes an uproar ratio.It is not present and is obscured using the azimuth that step 8 obtains, but precision is lower.As previously described, because step 7 second wave beam It is high to collect the azimuth accuracy that measures, but that there are angle measurements is fuzzy, i.e., can not determine azimuthal specific value, and what step 8 obtained Can to solve angle measurement fuzzy there is no fuzzy at azimuth, to obtain high Precision angle.For example, when there are 0, -41.8 for step 7 Degree, when the fuzzy angle such as 41.8 degree, it is 45 degree that pulse, which measures angle, although angle possibility precision is not high, is enough to solve survey Angle mould paste determines that the azimuth of step 7 is 41.8 degree.
Using the decoupling method of the millimetre-wave radar antenna system of four acceptors of above-mentioned three hair, target bearing can be calculated And pitch angle, and by the equivalent virtual array principle of MIMO, above-mentioned antenna system can fictionalize more receiving channels, raising side Parallactic angle Measurement Resolution.Using the monopulse antenna structure in the antenna system, can solve when receiving antenna interval is larger, Main beam shapes the fuzzy problem of azimuth angle measurement.
Those skilled in the art after considering the specification and implementing the invention disclosed here, will readily occur to of the invention its His embodiment.This application is intended to cover any variations, uses, or adaptations of the invention, these modifications, purposes or The variation of fit+answering property follow general principle of the invention and including the undocumented common knowledge in the art of the present invention or Conventional techniques.The description and examples are only to be considered as illustrative, and true scope and spirit of the invention are by claim It points out.

Claims (10)

1. a kind of millimetre-wave radar antenna system, it is characterised in that: including aerial array, primary processor and baseband processing circuitry, The aerial array includes at least 2 transmitting antennas and at least 2 receiving antennas, and the transmitting signal of primary processor is by transmitting day To object, receiving antenna is received by object reflected signal beta radiation, the signal after primary processor is mixed, Each target component is obtained by baseband processing circuitry analytical calculation.
2. a kind of millimetre-wave radar antenna system as described in claim 1, it is characterised in that: every transmitting antenna includes At least one linear array;The every receiving antenna includes at least one linear array.
3. a kind of millimetre-wave radar antenna system as described in claim 1, it is characterised in that: the linear array includes several patches Piece, the patch are the patch that width is weighted.
4. a kind of millimetre-wave radar antenna system as described in claim 1, it is characterised in that: the aerial array includes 3 Transmitting antenna and 4 receiving antennas.
5. a kind of millimetre-wave radar antenna system as claimed in claim 4, it is characterised in that: the aerial array includes successively The first transmitting antenna for being arranged, the second transmitting antenna, the first receiving antenna, the second receiving antenna, third receiving antenna, the 4th connect Receive antenna and third transmitting antenna;Wherein, the cross of the first the second receiving antenna of receiving antenna distance and third receiving antenna center D is divided intox3, wherein 3 λ≤dx3≤4.5λ;Lateral separation d between second receiving antenna, third receiving antennax4=0.5 λ, the lateral separation d of the 4th the second receiving antenna of receiving antenna distance and third receiving antenna centerx5=dx3, first hair Penetrate the lateral separation d between antenna, the second transmitting antennax1=dx3/ 2, longitudinal gap dy1=1.4 λ, the second transmitting antenna and Lateral separation d between three transmitting antennasx2=3dx3, longitudinal gap 0;Wherein the λ is carrier wavelength.
6. a kind of millimetre-wave radar antenna decoupling method, it is characterised in that include the following steps:
1) each transmitting antenna in aerial array emits signal simultaneously, with phase, and signal is after object reflects, by each reception Antenna receives;
2) equivalent virtually to obtain the virtual antenna array being made of N receiving antenna, N according to the equivalent virtual array principle of MIMO For the product of practical receiving antenna quantity and number of transmission antennas;
3) phase value at each receiving antenna center in virtual antenna array is calculated according to formula (1):
Wherein n=1,2,3 ... N, dazFor the horizontal spacing between each receiving antenna of virtual antenna array, delFor virtual antenna array Longitudinal pitch between each receiving antenna, λ are carrier wavelength, and θ is azimuth of target, and φ is pitch angle, obtain virtual antenna arrays Total phase set of receiving antenna in column
4) each phase value in total phase set is arranged to by several subsets according to function difference, the subset includes master Beam collectionFirst wavelet constrictionSecond wavelet constrictionWith pulse collectionIn wherein one or more;
5) to the main beam collectionPower estimation calculation is carried out, azimuth of target θ is obtained1;To the first beamletCollection carries out spectrum and estimates It calculates, obtains pitch angle φ;To the second wavelet constrictionPower estimation calculation is carried out, azimuth of target θ is obtained2, to the pulse CollectionUsing than phase algorithm, obtain without fuzzy azimuth.
7. a kind of millimetre-wave radar antenna decoupling method as claimed in claim 6, it is characterised in that: the main beam collection
8. a kind of millimetre-wave radar antenna decoupling method as claimed in claim 6, it is characterised in that: the first wavelet constrictionIncluding total phase setEach phase value of middle front half, i.e.,
9. a kind of millimetre-wave radar antenna decoupling method as claimed in claim 6, it is characterised in that: the second wavelet constrictionIncluding total phase setEach phase value when middle n is even number, i.e.,
10. a kind of millimetre-wave radar antenna decoupling method as claimed in claim 6, it is characterised in that: the pulse collection Including being divided into each phase value corresponding to the virtual receiving antenna of 0.5 λ between two.
CN201910014117.8A 2019-01-08 2019-01-08 A kind of millimetre-wave radar antenna system and decoupling method Pending CN109444891A (en)

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CN114204282A (en) * 2021-12-07 2022-03-18 中国电子科技集团公司第十四研究所 Large-scale array antenna based on virtual array
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CN115421134A (en) * 2022-08-15 2022-12-02 赛恩领动(上海)智能科技有限公司 Method and device for resolving ambiguity of radar speed and millimeter wave radar
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