CN102521472B - Method for constructing thinned MIMO (Multiple Input Multiple Output) planar array radar antenna - Google Patents

Method for constructing thinned MIMO (Multiple Input Multiple Output) planar array radar antenna Download PDF

Info

Publication number
CN102521472B
CN102521472B CN 201210000517 CN201210000517A CN102521472B CN 102521472 B CN102521472 B CN 102521472B CN 201210000517 CN201210000517 CN 201210000517 CN 201210000517 A CN201210000517 A CN 201210000517A CN 102521472 B CN102521472 B CN 102521472B
Authority
CN
China
Prior art keywords
array element
array
emission
centerdot
receiving
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 - Fee Related
Application number
CN 201210000517
Other languages
Chinese (zh)
Other versions
CN102521472A (en
Inventor
张晓玲
向高
师君
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.)
University of Electronic Science and Technology of China
Original Assignee
University of Electronic Science and Technology of China
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 University of Electronic Science and Technology of China filed Critical University of Electronic Science and Technology of China
Priority to CN 201210000517 priority Critical patent/CN102521472B/en
Publication of CN102521472A publication Critical patent/CN102521472A/en
Application granted granted Critical
Publication of CN102521472B publication Critical patent/CN102521472B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

The invention provides a method for constructing a thinned MIMO (Multiple Input Multiple Output) planar array radar antenna, which is on the basis of a phase center approximation principle and combines an MIMO antenna thought. The antenna arrangement optimal design is carried out by adopting the MIMO antenna thought. When all transmitting array elements simultaneously (or in turns) transmit orthogonal signals and receiving array elements simultaneously receive echo signals, a virtual planar array with uniform intervals is subjected to equivalence processing by utilizing the phase center approximation principle. According to the thinned MIMO planar array radar antenna constructed according to the invention, few transmitting antenna array elements and few receiving antenna array elements can be adopted and the equivalent full-array-element arrangement planar antenna array is virtually realized. Compared with the planar array antenna which is the same size as the equivalent virtual planar array and is directly arranged, the thinned MIMO planar array radar antenna constructed according to the method disclosed by the invention has the advantage of greatly reducing the requirement on the number of the array elements.

Description

A kind of sparse MIMO planar array radar antanna construction method
Technical field:
The invention belongs to the Radar Technology field, it has been particularly related to MIMO radar and radar array antenna technical field.
Technical background:
MIMO(Multiple-Input Multiple-Output) technology is proposed by Bell Laboratory the earliest, has been widely used at present wireless communication field, has effectively improved wireless coverage and data transmission performance.And the MIMO radar is a kind of New Type Radar system that just proposes the beginning of this century, compares the resource that the MIMO radar has utilized the emission battle array more with traditional radar, by launching many waveforms uncorrelated or that part is relevant, to obtain the waveform diversity gain; Also can arrange by the large array element interval of sending and receiving bay, make emitting electromagnetic wave shine from different perspectives target, thereby obtain space diversity gain.
The document of understanding and having delivered according to the inventor, for example: J.Klare, " Digital Beamforming for a3D MIMO SAR-Improvements through Frequency and Waveform Diversity; " in Geoscience and Remote Sensing Symposium, 2008.IGARSS2008.IEEE International, 2008, pp.V-17-V-20.There has been at present the people that MIMO array antenna technology is applied in the aspects such as linear-array three-dimensional imaging synthetic aperture radars, shown that the MIMO technology is in the feasibility of radar imagery field application.
Planar array antenna has important application in phased-array radar, can realize multiple goal is followed the tracks of and the navigate missile guidance fast; Can easily realize wave beam forming by changing phase weighting; Utilize planar array to have the space two-dimensional angular resolution, can also realize the three-dimensional radar imaging in conjunction with pulse compression technique.Yet for fear of graing lobe effect and the larger spacescan scope of realization, planar array antenna needs arrange according to full array element, causes the thousands of dual-mode antenna array element of needs and corresponding antenna control module, and cost is extremely expensive.Therefore, the optimal design of planar array antenna reduces its cost, becomes one of key issue that its widespread use needs to be resolved hurrily.
Summary of the invention:
The present invention has been mainly and has solved the problem that planar array antenna needs a large amount of bays, utilizes phase center to be similar to (PCA, Phase Center Approximation) and MIMO technology, has proposed a kind of sparse MIMO planar array radar antanna construction method.Can realize with less emitting antenna array element and receiving antenna array element the planar antenna array that the full array element of Virtual Realization equivalence is arranged according to the sparse MIMO planar array radar antanna that the present invention builds.
Content of the present invention for convenience of description, at first make following term definition:
Definition 1, MIMO radar
The full name of MIMO radar is " MIMO radar " (Multiple-Input Multiple-Output Radar), broadly the MIMO radar is defined as transmitting terminal and receiving end has a plurality of antennas, and the radar of a plurality of uncorrelated or part coherent signal waveforms of transmitting terminal emission.See document D.W. Bliss and K.W.Forsythe for details, " Multiple-input multiple-output (MIMO) radar and imaging:degrees of freedom and resolution; " in Signals, Systems and Computers, 2003.Conference Record of the Thirty-SeventhAsilomar Conference on, 2003, pp.54-59Vol.1.
Definition 2, orthogonal signal
The covariance of two signals is zero, claims them mutually orthogonal; If it is zero that an average is arranged in two signals, add up so uncorrelated and orthogonal equivalence.See document " the modern digital signal is processed and used " for details, He Zishu etc. write, publishing house of Tsing-Hua University, 2009.
Definition 3, space diversity
Space diversity be a kind of transmitting terminal or (with) receiving end installs the diversity technique of the antenna of many diverse locations.If the distance of these antenna is enough large, the impact that declined of electromagnetic wave is just separate.See document " present mobile communication " for details, Pang Baomao etc., publishing house of Tsing-Hua University, 2004.
Definition 4, waveform diversity
Waveform diversity refers to by the various parameters of reasonable design transmitted waveform and the related coefficient between waveform, system performance be maximized.See document " performance evaluation that single base MIMO radar DOA estimates " for details, Yang Wei, Xian Electronics Science and Technology University, 2009.
Definition 5, installation rectangle plane
Rectangle plane being installed being referred to the fixed pan that planar array antenna is mounted, is a rectangle.As shown in Figure 1.
Definition 6, planar array antenna
Planar array antenna refers to that antenna sending and receiving array element all is installed in a fixed pan, and array element is according to rectangle or rounded projections arranged usually.See document " radar handbook (second edition) " for details, Wang Jun etc. translate, the Electronic Industry Press.
The coordinate system of definition 7, installation rectangle plane
The coordinate system of rectangle plane is installed true origin is set the center that rectangle plane is installed, coordinate axis x is parallel with two adjacent edges that rectangle plane is installed respectively with coordinate axis y, sets up coordinate system with right-handed system, as shown in Figure 1.See document " linear algebra and space analytic geometry (second edition) " for details, the work such as Huang Tingzhu, Higher Education Publishing House, 2003.
The definition 8, planar array antenna horizontal and vertical
Laterally referring in the x-direction of planar array antenna; Planar array antenna vertically refer to direction along y.As shown in Figure 1.
Definition 9, planar array antenna beam pattern
The spatial filtering response of planar array antenna is the planar array antenna beam pattern, when array is input as plane wave, and the relation between battle array output (usually only considering output amplitude or power) and plane incident angle.See document " auto adapted filtering---self-adaptive filters in time area and smart antenna " for details, Gong Yaohuan, second edition, Electronic Industry Press, 2003.
Lateral angle resolution and the longitudinal angle resolution of definition 10, planar array antenna
The lateral angle resolution of planar array antenna refers to by the pattern of transmitting antenna center, carries out in the x-direction vertical section, and the 3dB width of section main lobe is used Expression; The longitudinal angle resolution of planar array antenna refers to by the pattern of transmitting antenna center, carries out in the y-direction vertical section, and the 3dB width of section main lobe is used
Figure GDA00002739778500032
Expression.See document " auto adapted filtering---self-adaptive filters in time area and smart antenna " for details, Gong Yaohuan, second edition, Electronic Industry Press, 2003.
Definition 11, emitting antenna array element and receiving antenna array element
Emitting antenna array element refers to be arranged on planar array antenna, for the bay of the waveform that transmits, is called for short emission array element, represents with T; Receiving antenna array element refers to be arranged on planar array antenna, is used for receiving the bay of echoed signal, is called for short receiving array element, represents with R.As shown in Figure 1.
Horizontal spacing and longitudinal pitch between definition 12, emitting antenna array element
Between emitting antenna array element, horizontal spacing refers to the spacing that emitting antenna array element distributes in the x-direction, uses d xTExpression; Between emitting antenna array element, longitudinal pitch refers to the spacing that emitting antenna array element distributes in the y-direction, uses d yTExpression.As shown in Figure 1.
Horizontal spacing and longitudinal pitch between definition 13, receiving antenna array element
Between receiving antenna array element, horizontal spacing refers to the spacing that receiving antenna array element distributes in the x-direction, uses d xRExpression; Between receiving antenna array element, longitudinal pitch refers to the spacing that receiving antenna array element distributes in the y-direction, uses d yRExpression.As shown in Figure 1.
Horizontal spacing and longitudinal pitch between definition 14, sending and receiving bay
Between the sending and receiving bay, horizontal spacing refers to the spacing that adjacent receiving antenna array element and emitting antenna array element distribute in the x-direction, uses d xTRExpression; Between the sending and receiving bay, longitudinal pitch refers to the spacing that adjacent receiving antenna array element and emitting antenna array element distribute in the y-direction, uses d yTRExpression.As shown in Figure 1.
Definition 15, approximate (PCA) principle of phase center
The approximate principle of phase center is thought: under far field condition (namely
Figure GDA00002739778500041
L wherein TRFor receiving the spacing between array element and emission array element, r is for emission array element and receive the centre position of array element to the distance of scattering point, λ is signal wavelength), a pair of bay that splits that transmits and receives can be replaced by the displaced phase center of a transmit-receive sharing that is positioned at their centers.Detailed content can be with reference to Bellettini A, Pinto M A, " Theoretical Accuracy of Synthetic Aperture Sonar Micronavigation Using a Displaced Phase Center Antenna " .IEEE Journal of Oceanic Engineering, 2002; Vol.27, No.4, pp.780-789.
Definition 16, Virtual array, virtual linear array and virtual plane array
Principle approximate according to phase center, under far field condition, a pair of bay that splits that transmits and receives can be replaced by the displaced phase center of a transmit-receive sharing that is positioned at their centers, and the displaced phase center of this transmit-receive sharing is Virtual array; All Virtual arrays are arranged according to certain position relationship and are virtual linear array point-blank; All virtual linear arrays are arranged in a rectangle according to certain position relation and are the virtual plane array.As shown in Figures 2 and 3.Detailed content can be with reference to Ilya Bekkerman and Joseph Tabrikian. " Target Detection and Localization Using MIMO Radars and Sonars " .IEEE Transactions on signal processing, 2006,54 (10): 3873 ~ 3883.
Lateral length and the longitudinal length of definition 17, virtual plane array
The lateral length of virtual plane array refers to that the virtual plane array along the length that the x axle distributes, uses L vxExpression; The longitudinal length of virtual plane array refers to that the virtual plane array along the length that the y axle distributes, uses L vyExpression.As shown in Figure 3.
Horizontal spacing and longitudinal pitch between definition 18, virtual plane array array element
Horizontal spacing between virtual plane array array element refers between virtual plane array array element to use d along the spacing of x axle vxExpression; Longitudinal pitch between virtual plane array array element refers between virtual plane array array element to use d along the spacing of y axle vyExpression.As shown in Figure 3.
Define 19, round up
The mathematical definition that rounds up is
Figure GDA00002739778500051
The smallest positive integral that is not less than s is got in expression, and wherein, ∈ is for belonging to symbol,
Figure GDA00002739778500052
The set of expression integer, The expression real number set, n represents arbitrary integer, s represents any real number.
Definition 20, upwards get idol
Upwards getting even mathematical definition is
Figure GDA00002739778500054
The minimum even number that is not less than s is got in expression, and wherein, ∈ is for belonging to symbol,
Figure GDA00002739778500055
The set of expression even number, The expression real number set, n represents any even number, s represents any real number.
Spacing between definition 21, array element
Between array element, spacing comprises horizontal spacing between emission array element, and longitudinal pitch between emission array element receives horizontal spacing between array element, receives longitudinal pitch between array element, longitudinal pitch between horizontal spacing and sending and receiving array element between sending and receiving array element.
The present invention proposes a kind of sparse MIMO planar array radar antanna construction method, the specific implementation step of the method is as follows:
The initialization setting of step 1, antenna correlation parameter
At first, determine the dimensional parameters of virtual plane array.The lateral angle resolution of given planar array antenna
Figure GDA00002739778500057
Differentiate with longitudinal angle
Figure GDA00002739778500058
Calculate the lateral length L of virtual plane array vxLength L longitudinally vyDescribe with mathematical formulae:
Figure GDA00002739778500059
With
Figure GDA000027397785000510
Wherein the radar signal carrier wavelength lambda is known.
Secondly, determine horizontal spacing and longitudinal pitch between virtual plane array array element.Horizontal spacing d between virtual plane array array element vxExpression, the longitudinal pitch d between virtual plane array array element vyExpression.Regulation is respectively θ along the maximum field angle of x and scanning in the y-direction x0And θ y0, according to the graing lobe formula With Determine d vxAnd d vySpan, symbol || the expression computing that takes absolute value.Select With
Figure GDA000027397785000514
Can realize along x and in the y-direction scanning field angle from
Figure GDA000027397785000515
Arrive
Figure GDA000027397785000516
The beam scanning scope.
Again, determine that the array element of virtual plane array is along x to the columns N that arranges vxWith along y to the array element line number N that arranges vy:
Figure GDA00002739778500061
Symbol wherein
Figure GDA00002739778500063
Representative rounds up, and the smallest positive integral that is not less than " " is got in expression.
At last, determine to build the emission array element number M that the virtual plane array needs TWith reception array element number N RDetailed process is as follows:
(1), building array element number is N vxVirtual linear array: namely determine the emission array element number and receive array element number
Use M xTThe emission array element number that expression needs, and regulation M xTBe even number, use N xRThe reception array element number that expression needs is used c TAnd c RExpression is laid an emission array element with the reception needed cost of array element (cost refers to the expense of bay, processing and installation) and for known herein, respectively.Choose
Figure GDA00002739778500064
Wherein
Figure GDA00002739778500065
Idol is upwards got in representative, and the minimum even number that is not less than " " is got in expression;
Figure GDA00002739778500066
Wherein
Figure GDA00002739778500067
Representative rounds up, and the smallest positive integral that is not less than " " is got in expression.
(2), building array element number is N vyVirtual linear array: namely determine the emission array element number and receive array element number
Use M yTThe emission array element number that expression needs, and regulation M yTBe even number; Use N yRThe reception array element number that expression needs.Choose
Figure GDA00002739778500068
Figure GDA00002739778500069
So the structure array element number is N vy* N vxThe virtual plane array, needed emission array element number M T=M xT* M yT, the reception array element number that needs is N R=N xR* N yR
Step 2, determine spacing between array element
Horizontal spacing d between emission array element xT: d xT=2d vx, d vxBe the horizontal spacing between virtual plane array array element;
Longitudinal pitch d between emission array element yT: d yT=2d vy, d vyBe the longitudinal pitch between virtual plane array array element;
Receive horizontal spacing d between array element xR: d vxBe the horizontal spacing between virtual plane array array element, M xTBe N for building array element number vxThe emission array element number that needs of virtual linear array;
Receive longitudinal pitch d between array element yR:
Figure GDA00002739778500072
d vyBe the longitudinal pitch between virtual plane array array element, M yTBe N for building array element number vyThe emission array element number that needs of virtual linear array;
Horizontal spacing d between sending and receiving array element xTR:
Figure GDA00002739778500073
d vxBe the horizontal spacing between virtual plane array array element, d xTBe horizontal spacing between emission array element;
Longitudinal pitch d between sending and receiving array element yTR:
Figure GDA00002739778500074
d vyBe the longitudinal pitch between virtual plane array array element, d yTBe longitudinal pitch between emission array element;
Step 3, definite coordinate system that rectangle plane is installed
The center that rectangle plane is installed is defined as true origin, and the x axle is parallel with installation rectangle plane adjacent two edges respectively with the y axle, sets up the planar coordinate system.As shown in Figure 1.
Step 4, layout receive array element
Receive the total N of array element RIndividual, each receives the position coordinates of array element and determines according to following formula:
Receive array element horizontal ordinate x R(i):
Figure GDA00002739778500075
I={1,2 ..., N xR, N xRBe N for building array element number vxThe reception array element number that needs of virtual linear array, d xRFor receiving horizontal spacing between array element;
Receive array element ordinate y R(k):
Figure GDA00002739778500076
K={1,2 ..., N yR, N yRBe N for building array element number vyThe reception array element number that needs of virtual linear array, d yRFor receiving longitudinal pitch between array element.
Step 5, layout emission array element
The total M of emission array element TIndividual, be divided into about centrosymmetric four parts of initial point (I, II, III and IV, as shown in Figure 1) in, every part has emission array element
Figure GDA00002739778500081
Individual.Determine respectively the position coordinates of every part emission array element:
(1), part i emission array element
The horizontal ordinate x of part i emission array element T_I(i):
x T _ I ( i ) = ( i - M xT 2 ) d xT + ( 1 - N xR 2 ) d xR - d xTR , i = { 1,2 , · · · , M xT 2 } , M xTAnd N xRBeing respectively and building array element number is N vxThe emission array element number that needs of virtual linear array and receive array element number, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
The ordinate y of part i emission array element T_I(k):
y T _ I ( k ) = ( M yT 2 - k ) d yT + ( N yR - 1 2 ) d yR + d yTR , k = { 1,2 , · · · , M yT 2 } , M yTAnd N yRBeing respectively and building array element number is N vyThe emission array element number that needs of virtual linear array and receive array element number, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element;
(2), part ii emission array element
The horizontal ordinate x of part ii emission array element T_II(i):
x T _ II ( i ) = ( M xT 2 - i ) d xT + ( N xR - 1 2 ) d xR + d xTR , i = { 1,2 , · · · , M xT 2 } , M xTAnd N xRBeing respectively and building array element number is N vxThe emission array element number that needs of virtual linear array and receive array element number, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
The ordinate y of part ii emission array element T_II(k):
y T _ II ( k ) = ( M yT 2 - k ) d yT + ( N yR - 1 2 ) d yR + d yTR , k = { 1,2 , · · · , M yT 2 } , M yTAnd N yRBeing respectively and building array element number is N vyThe emission array element number that needs of virtual linear array and receive array element number, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element;
(3), III partly launches array element
III partly launches the horizontal ordinate x of array element T_III(i):
x T _ III ( i ) = ( i - M xT 2 ) d xT + ( 1 - N xR 2 ) d xR - d xTR , i = { 1,2 , · · · , M xT 2 } , M xTAnd N xRBeing respectively and building array element number is N vxThe emission array element number that needs of virtual linear array and receive array element number, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
III partly launches the ordinate y of array element T_III(k):
y T _ III ( k ) = ( k - M yT 2 ) d yT + ( 1 - N yR 2 ) d yR - d yTR , k = { 1,2 , · · · , M yT 2 } , M yTAnd N yRBeing respectively and building array element number is N vyThe emission array element number that needs of virtual linear array and receive array element number, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element;
(4), IV partly launches array element
IV partly launches the horizontal ordinate x of array element T_IV(i):
x T _ IV ( i ) = ( M xT 2 - i ) d xT + ( N xR - 1 2 ) d xR + d xTR , i = { 1,2 , · · · , M xT 2 } , M xTAnd N xRBeing respectively and building array element number is N vxThe emission array element number that needs of virtual linear array and receive array element number, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
IV partly launches the ordinate y of array element T_IV(k):
y T _ IV ( k ) = ( k - M yT 2 ) d yT + ( 1 - N yR 2 ) d yR - d yTR , k = { 1,2 , · · · , M yT 2 } , M yTAnd N yRBeing respectively and building array element number is N vyThe emission array element number that needs of virtual linear array and receive array element number, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element.
Arrange according to the position coordinates that receives element position coordinate and four parts of emission array element, just consisted of sparse MIMO planar array radar antanna of the present invention.
Need to prove that the present invention arranges mainly for emission array element and the geometry that receives array element carries out array optimization, when all emission array elements whiles (or in turn) emission orthogonal signal, and when receiving array element and receiving echoed signal simultaneously, utilize method equivalence of the present invention to go out to have evenly spaced virtual plane array.
Innovative point of the present invention is in conjunction with the MIMO antenna concept, to have invented a kind of sparse MIMO planar array radar antanna building method take the approximate principle of phase center as the basis.
The invention has the advantages that and adopt on the one hand MIMO thought to carry out the antenna optimal design of structuring the formation, when all emission array elements whiles (or in turn) emission orthogonal signal, and when receiving array element and receiving echoed signal simultaneously, utilize the approximate principle of phase center equivalence to go out to have evenly spaced virtual plane array; On the other hand, compare with the onesize planar array antenna of virtual plane array of equivalence with direct laying, method for designing of the present invention has greatly reduced the demand to array element number.
Description of drawings
The sparse MIMO planar array radar antanna of Fig. 1 scheme of installation
Wherein, rectangle plane is installed in " 1 " representative; I, II, III and IV represent respectively four groups of emitting antenna array elements of sparse MIMO planar array; " " representative emission array element T, " zero " representative receives array element R; d xTAnd d yTHorizontal spacing and the longitudinal pitch between array element launched in expression respectively; d xRAnd d yRExpression receives horizontal spacing and the longitudinal pitch between array element respectively; d xTRAnd d yTRRepresent respectively horizontal spacing and longitudinal pitch between sending and receiving array element; X and y represent respectively to install x axle and the y axle of the coordinate system of rectangle plane; O represents to install the initial point of the coordinate system of rectangle plane.
The virtual linear array schematic diagram of Fig. 2
Wherein, " " representative emission array element T, " zero " representative receives array element R, and " ■ " represents Virtual array.
Fig. 3 virtual plane array schematic diagram
Wherein, d vxAnd d vyRepresent respectively horizontal spacing and longitudinal pitch between virtual plane array array element; L vxAnd L vyThe lateral length and the longitudinal length that represent respectively the virtual plane array; N vxAnd N vyThe array element columns and the line number that represent respectively the virtual plane array; " ■ " represents Virtual array, and x and y represent respectively to install x axle and the y axle of the coordinate system of rectangle plane; O represents to install the initial point of the coordinate system of rectangle plane.
Fig. 4 FB(flow block) of the present invention
Embodiment:
The initialization setting of step 1, antenna correlation parameter
At first, determine the dimensional parameters of virtual plane array.The lateral angle resolution of given planar array antenna
Figure GDA00002739778500111
Differentiate with longitudinal angle Radar signal carrier wavelength lambda=0.03m.Calculate the lateral length of virtual plane array
Figure GDA00002739778500113
Length longitudinally
Figure GDA00002739778500114
Secondly, determine horizontal spacing and longitudinal pitch between virtual plane array array element.Horizontal spacing d between virtual plane array array element vxExpression, the longitudinal pitch d between virtual plane array array element vyExpression.Regulation is respectively along the maximum field angle of x and scanning in the y-direction
Figure GDA00002739778500115
With
Figure GDA00002739778500116
According to the graing lobe formula 0 < d vx &le; &lambda; 1 + | sin &theta; x 0 | With 0 < d vy &le; &lambda; 1 + | sin &theta; y 0 | Determine d vxAnd d vySpan, symbol || the expression computing that takes absolute value.Select d vx=0.015m and d vy=0.015m.
Again, determine that the array element of virtual plane array is along x to the columns N that arranges vxWith along y to the array element line number N that arranges vy:
Figure GDA00002739778500119
Figure GDA000027397785001110
Symbol wherein
Figure GDA000027397785001111
Representative rounds up, and the smallest positive integral that is not less than " " is got in expression.
At last, determine to realize the emission array element number M of virtual plane array needs TWith reception array element number N R
Detailed process is as follows:
(1), building array element number is N vxVirtual linear array: namely determine the emission array element number and receive array element number
Use M xTThe emission array element number that expression needs, and regulation M xTBe even number, use N xRThe reception array element number that expression needs, get install an emission array element with one to receive array element cost (, cost refers to the expense of bay, processing and installation) herein identical, i.e. c T=c RChoose
Figure GDA00002739778500121
Wherein
Figure GDA00002739778500122
Idol is upwards got in representative, and the minimum even number that is not less than " " is got in expression;
Figure GDA00002739778500123
Wherein
Figure GDA00002739778500124
Representative rounds up, and the smallest positive integral that is not less than " " is got in expression.
(2), building array element number is N vyVirtual linear array: namely determine the emission array element number and receive array element number
Use M yTThe emission array element number that expression needs, and regulation M yTBe even number; Use N yRThe reception array element number that expression needs.Choose
Figure GDA00002739778500125
Figure GDA00002739778500126
So the structure array element number is N vy* N vxThe virtual plane array, needed emission array element number M T=M xT* M yT=36, the reception array element number that needs is N R=N xR* N yR=36.
Step 2, determine spacing between array element
Horizontal spacing d between emission array element xT: d xT=2d vx=0.03m, d vxBe the horizontal spacing between virtual plane array array element;
Longitudinal pitch d between emission array element yT: d yT=2d vy=0.03m, d vyBe the longitudinal pitch between virtual plane array array element;
Receive horizontal spacing d between array element xR:
Figure GDA00002739778500127
d vxBe the horizontal spacing between virtual plane array array element, M xTBe N for building array element number vxThe emission array element number that needs of virtual linear array;
Receive longitudinal pitch d between array element yR:
Figure GDA00002739778500128
d vyBe the longitudinal pitch between virtual plane array array element, M yTBe N for building array element number vyThe emission array element number that needs of virtual linear array;
Horizontal spacing d between sending and receiving array element xTR:
Figure GDA00002739778500131
d vxBe the horizontal spacing between virtual plane array array element, d xTBe horizontal spacing between emission array element;
Longitudinal pitch d between sending and receiving array element yTR:
Figure GDA00002739778500132
d vyBe the longitudinal pitch between virtual plane array array element, d yTBe longitudinal pitch between emission array element;
Step 3, definite coordinate system that rectangle plane is installed
The center that rectangle plane is installed is defined as true origin, and the x axle is parallel with installation rectangle plane adjacent two edges respectively with the y axle, sets up the planar coordinate system.As shown in Figure 1.
Step 4, layout receive array element
Receive array element and have 36, each receives the position coordinates of array element and determines according to following formula:
Receive array element horizontal ordinate x R(i):
Figure GDA00002739778500133
I={1,2 ..., 6}, d xRFor receiving horizontal spacing between array element;
Receive array element ordinate y R(k):
Figure GDA00002739778500134
K={1,2 ..., 6}, d yRFor receiving longitudinal pitch between array element;
Step 5, layout emission array element
Emission array element has 36, is divided into that (I, II, III and IV, as shown in Figure 1), every part has 9 of array elements of emission about centrosymmetric four parts of initial point.Determine respectively the position coordinates of every part emission array element:
(1), part i emission array element
The horizontal ordinate x of part i emission array element T_I(i):
x T _ I ( i ) = ( i - 3 ) d xT - 5 2 d xR - d xTR , I={1,2,3}, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
The ordinate y of part i emission array element T_I(k):
y T _ I ( k ) = ( 3 - k ) d yT - 5 2 d yR + d yTR , K={1,2,3}, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element;
(2), part ii emission array element
The horizontal ordinate x of part ii emission array element T_II(i):
x T _ II ( i ) = ( 3 - i ) d xT + 5 2 d xR + d xTR , I={1,2,3}, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
The ordinate y of part ii emission array element T_II(k):
y T _ II ( k ) = ( 3 - k ) d yT + 5 2 d yR + d yTR , K={1,2,3}, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element;
(3), III partly launches array element
III partly launches the horizontal ordinate x of array element T_III(i):
x T _ III ( i ) = ( i - 3 ) d xT - 5 2 d xR - d xTR , I={1,2,3}, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
III partly launches the ordinate y of array element T_III(k):
y T _ III ( k ) = ( k - 3 ) d yT - 5 2 d yR - d yTR , k = { 1,2,3 } , d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element;
(4), IV partly launches array element
IV partly launches the horizontal ordinate x of array element T_IV(i):
x T _ IV ( i ) = ( 3 - i ) d xT + 5 2 d xR + d xTR , I={1,2,3}, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
IV partly launches the ordinate y of array element T_IV(k):
y T _ IV ( k ) = ( k - 3 ) d yT - 5 2 d yR - d yTR , K={1,2,3}, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element.
Arrange according to the position coordinates that receives element position coordinate and four parts of emission array element, just consisted of sparse MIMO planar array radar antanna of the present invention, equivalence is the virtual plane array of a 0.54m * 0.54m.
Can find out by the specific embodiment of the invention, directly realize the planar array antenna of a 0.54m * 0.54m, needed bay number is 36 * 36=1296; Realize and pass through sparse MIMO planar array radar antanna construction method of the present invention, only need 36 emission array elements and 36 reception array elements, altogether add up to 72 bays; When arranging an emission array element and arranging that a reception array element cost is identical, cost so required for the present invention is approximately directly to realize
Figure GDA00002739778500151
Show that the present invention can reduce the cost of planar array antenna design greatly.

Claims (1)

1. sparse MIMO planar array radar antanna construction method is characterized in that it comprises the following steps:
The initialization setting of step 1, antenna correlation parameter
At first, determine the dimensional parameters of virtual plane array; The lateral angle resolution of given planar array antenna
Figure FDA00002739778400011
Differentiate with longitudinal angle
Figure FDA00002739778400012
Calculate the lateral length L of virtual plane array vxLength L longitudinally vyDescribe with mathematical formulae:
Figure FDA00002739778400013
With
Figure FDA00002739778400014
Wherein the radar signal carrier wavelength lambda is known;
Secondly, determine horizontal spacing and longitudinal pitch between virtual plane array array element; Horizontal spacing d between virtual plane array array element vxExpression, the longitudinal pitch d between virtual plane array array element vyExpression; Regulation is respectively θ along the maximum field angle of x and scanning in the y-direction x0And θ y0, according to the graing lobe formula
Figure FDA00002739778400015
With
Figure FDA00002739778400016
Determine d vxAnd d vySpan, symbol || the expression computing that takes absolute value; Select With
Figure FDA00002739778400018
Can realize along x and in the y-direction scanning field angle from
Figure FDA00002739778400019
Arrive
Figure FDA000027397784000110
The beam scanning scope;
Again, determine that the array element of virtual plane array is along x to the columns Nvx that arranges with along y to the array element line number N that arranges vy:
Figure FDA000027397784000111
Figure FDA000027397784000112
Symbol wherein
Figure FDA000027397784000113
Representative rounds up, and the smallest positive integral that is not less than " " is got in expression;
At last, determine to build the emission array element number M that the virtual plane array needs TWith reception array element number N RDetailed process is as follows:
(1), building array element number is N vxVirtual linear array: namely determine the emission array element number and receive array element number
Use M xTThe emission array element number that expression needs, and regulation M xTBe even number, use N xRThe reception array element number that expression needs is used c TAnd c RExpression is laid an emission array element and is received the needed cost of array element respectively, and cost refers to the expense of bay, processing and installation, and is known; Choose
Figure FDA000027397784000114
Wherein
Figure FDA00002739778400021
Idol is upwards got in representative, and the minimum even number that is not less than " " is got in expression;
Figure FDA00002739778400022
Wherein
Figure FDA00002739778400023
Representative rounds up, and the smallest positive integral that is not less than " " is got in expression;
(2), building array element number is N vyVirtual linear array: namely determine the emission array element number and receive array element number
Use M yTThe emission array element number that expression needs, and regulation M yTBe even number; Use N yRThe reception array element number that expression needs; Choose
Figure FDA00002739778400025
So the structure array element number is N vy* N vxThe virtual plane array, needed emission array element number M T=M xT* M yT, the reception array element number that needs is N R=N xR* N yR
Step 2, determine spacing between array element
Horizontal spacing d between emission array element xT: d xT=2d vx, d vxBe the horizontal spacing between virtual plane array array element;
Longitudinal pitch d between emission array element yT: d yT=2d vy, d vyBe the longitudinal pitch between virtual plane array array element;
Receive horizontal spacing d between array element xR: d vxBe the horizontal spacing between virtual plane array array element, M xTBe N for building array element number vxThe emission array element number that needs of virtual linear array;
Receive longitudinal pitch d between array element yR:
Figure FDA00002739778400027
d vyBe the longitudinal pitch between virtual plane array array element, M yTBe N for building array element number vyThe emission array element number that needs of virtual linear array;
Horizontal spacing d between sending and receiving array element xTR:
Figure FDA00002739778400028
d vxBe the horizontal spacing between virtual plane array array element, d xTBe horizontal spacing between emission array element;
Longitudinal pitch d between sending and receiving array element yTR:
Figure FDA00002739778400029
d vyBe the longitudinal pitch between virtual plane array array element, d yTBe longitudinal pitch between emission array element;
Step 3, definite coordinate system that rectangle plane is installed
The center that rectangle plane is installed is defined as true origin, and the x axle is parallel with installation rectangle plane adjacent two edges respectively with the y axle, sets up the planar coordinate system;
Step 4, layout receive array element
Receive the total N of array element RIndividual, each receives the position coordinates of array element and determines according to following formula:
Receive array element horizontal ordinate x R(i): x R ( i ) = ( i - N xR + 1 2 ) d xR , I={1,2 ..., N xR, N xRBe N for building array element number vxThe reception array element number that needs of virtual linear array, d xRFor receiving horizontal spacing between array element;
Receive array element ordinate y R(k): y R ( k ) = ( k - N yR + 1 2 ) d yR , K={1,2 ..., N yR, N yRBe N for building array element number vyThe reception array element number that needs of virtual linear array, d yRFor receiving longitudinal pitch between array element;
Step 5, layout emission array element
The total M of emission array element TIndividual, be divided into about in centrosymmetric four parts of initial point: I, II, III and IV, every part has emission array element
Figure FDA00002739778400033
Individual; Determine respectively the position coordinates of every part emission array element:
(1), part i emission array element
The horizontal ordinate x of part i emission array element T_I(i):
x T _ I ( i ) = ( i - M xT 2 ) d xT + ( 1 - N xR 2 ) d xR - d xTR , i = { 1,2 , &CenterDot; &CenterDot; &CenterDot; , M xT 2 } , M xTAnd N xRBeing respectively and building array element number is N vxThe emission array element number that needs of virtual linear array and receive array element number, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
The ordinate y of part i emission array element T_I(k):
y T _ I ( k ) = ( M yT 2 - k ) d yT + ( N yR - 1 2 ) d yR + d yTR , k = { 1,2 , &CenterDot; &CenterDot; &CenterDot; , M yT 2 } , M yTAnd N yRBeing respectively and building array element number is N vyThe emission array element number that needs of virtual linear array and receive array element number, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element;
(2), part ii emission array element
The horizontal ordinate x of part ii emission array element T_II(i):
x T _ II ( i ) = ( M xT 2 - i ) d xT + ( N xR - 1 2 ) d xR + d xTR , i = { 1,2 , &CenterDot; &CenterDot; &CenterDot; , M xT 2 } , M xTAnd N xRBeing respectively and building array element number is N vxThe emission array element number that needs of virtual linear array and receive array element number, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
The ordinate y of part ii emission array element T_II(k):
y T _ II ( k ) = ( M yT 2 - k ) d yT + ( N yR - 1 2 ) d yR + d yTR , k = { 1,2 , &CenterDot; &CenterDot; &CenterDot; , M yT 2 } , M yTAnd N yRBeing respectively and building array element number is N xyThe emission array element number that needs of virtual linear array and receive array element number, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element;
(3), III partly launches array element
III partly launches the horizontal ordinate x of array element T_III(i):
x T _ III ( i ) = ( i - M xT 2 ) d xT + ( 1 - N xR 2 ) d xR - d xTR , i = { 1,2 , &CenterDot; &CenterDot; &CenterDot; , M xT 2 } , M xTAnd N xRBeing respectively and building array element number is N vxThe emission array element number that needs of virtual linear array and receive array element number, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
III partly launches the ordinate y of array element T_III(k):
y T _ III ( k ) = ( k - M yT 2 ) d yT + ( 1 - N yR 2 ) d yR - d yTR , k = { 1,2 , &CenterDot; &CenterDot; &CenterDot; , M yT 2 } , M yTAnd N yRBeing respectively and building array element number is N xyThe emission array element number that needs of virtual linear array and receive array element number, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element;
(4), IV partly launches array element
IV partly launches the horizontal ordinate x of array element T_IV(i):
x T _ IV ( i ) = ( M xT 2 - i ) d xT + ( N xR - 1 2 ) d xR + d xTR , i = { 1,2 , &CenterDot; &CenterDot; &CenterDot; , M xT 2 } , M xTAnd N xRBeing respectively and building array element number is N vxThe emission array element number that needs of virtual linear array and receive array element number, d xTBe horizontal spacing between emission array element, d xRFor receiving horizontal spacing between array element, d xTRBe horizontal spacing between sending and receiving array element;
IV partly launches the ordinate y of array element T_IV(k):
y T _ IV ( k ) = ( k - M yT 2 ) d yT + ( 1 - N yR 2 ) d yR - d yTR , k = { 1,2 , &CenterDot; &CenterDot; &CenterDot; , M yT 2 } , M yTAnd N yRBeing respectively and building array element number is N vyThe emission array element number that needs of virtual linear array and receive array element number, d yTBe longitudinal pitch between emission array element, d yRFor receiving longitudinal pitch between array element, d yTRBe longitudinal pitch between sending and receiving array element;
Arrange according to the position coordinates that receives element position coordinate and four parts of emission array element, consist of sparse MIMO planar array radar antanna.
CN 201210000517 2012-01-04 2012-01-04 Method for constructing thinned MIMO (Multiple Input Multiple Output) planar array radar antenna Expired - Fee Related CN102521472B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201210000517 CN102521472B (en) 2012-01-04 2012-01-04 Method for constructing thinned MIMO (Multiple Input Multiple Output) planar array radar antenna

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201210000517 CN102521472B (en) 2012-01-04 2012-01-04 Method for constructing thinned MIMO (Multiple Input Multiple Output) planar array radar antenna

Publications (2)

Publication Number Publication Date
CN102521472A CN102521472A (en) 2012-06-27
CN102521472B true CN102521472B (en) 2013-06-12

Family

ID=46292385

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201210000517 Expired - Fee Related CN102521472B (en) 2012-01-04 2012-01-04 Method for constructing thinned MIMO (Multiple Input Multiple Output) planar array radar antenna

Country Status (1)

Country Link
CN (1) CN102521472B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3522300A1 (en) * 2018-02-05 2019-08-07 The Boeing Company Axisymmetric thinned digital beamforming array for reduced power consumption

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102912054B (en) * 2012-11-13 2014-07-23 北京航空航天大学 Device for measuring material surface by using blast furnace based on multiple input multiple output (MIMO) radar
CN103197315B (en) * 2013-03-22 2014-10-15 电子科技大学 Flow structure non-uniform linear motion synthetic aperture radar imaging method
DE102013209708A1 (en) * 2013-05-24 2014-11-27 Robert Bosch Gmbh Method for operating a MIMO radar
CN103616667B (en) * 2013-11-20 2015-10-28 中国电子科技集团公司第四十一研究所 A kind of two-dimensional antenna array method for arranging for being scattering into picture
CN105765788B (en) * 2014-03-20 2018-10-09 华为技术有限公司 A kind of array antenna is structured the formation method, apparatus and array antenna
WO2015139294A1 (en) * 2014-03-21 2015-09-24 华为技术有限公司 Array antenna
CN103985970A (en) * 2014-04-28 2014-08-13 零八一电子集团有限公司 Distribution method capable of restraining grating lobes of large-space phased-array antenna
CN103969642B (en) * 2014-05-04 2016-05-25 中国电子科技集团公司第四十一研究所 A kind of phase compensating method for the imaging of many linear transducer arrays
EP2963442B1 (en) * 2014-07-04 2016-11-30 Denso Corporation Radar apparatus
CN104391276B (en) * 2014-10-08 2017-05-24 西安电子工程研究所 Transmit-receive split planar array phased-array radar antenna array and beam former
CN104269658B (en) * 2014-10-21 2016-04-27 内蒙古工业大学 For the arcuate array antenna of MIMO-SAR imaging
JP6377000B2 (en) * 2015-03-25 2018-08-22 パナソニック株式会社 Radar equipment
CN104849696B (en) * 2015-04-27 2017-04-19 中南大学 MIMO radar antenna array sparse arraying method
CN104898127A (en) * 2015-06-17 2015-09-09 西安电子科技大学 Multiple-input multiple-output synthetic aperture ladar system and system design method thereof
JP6755121B2 (en) * 2015-09-17 2020-09-16 パナソニック株式会社 Radar device
SE541664C2 (en) 2015-10-23 2019-11-19 Qamcom Tech Ab MIMO radar system and calibration method thereof
CN105490033B (en) * 2016-01-15 2018-01-02 中国电子科技集团公司第三十八研究所 A kind of L-shaped submatrix application method
CN105762533A (en) * 2016-04-15 2016-07-13 中国电子科技集团公司第三十八研究所 Eight-unit L-shaped subarray application method and application device based on modularization
US11454719B2 (en) * 2016-07-08 2022-09-27 Magna Electronics Inc. 2D MIMO radar system for vehicle
US20180159246A1 (en) * 2016-12-05 2018-06-07 GM Global Technology Operations LLC Modular architecture of the mimo radar
US11532869B2 (en) 2017-04-27 2022-12-20 Sony Corporation Radar antenna array for three-dimensional imaging
CN109696709B (en) * 2017-10-20 2020-12-04 中国工程物理研究院电子工程研究所 One-dimensional sparse array structure for human body security inspection imaging and design method thereof
CN108226871B (en) * 2018-01-18 2021-08-10 西安电子工程研究所 Diversity phased array design method based on millimeter wave collision avoidance radar
CN108761954B (en) * 2018-04-18 2020-02-28 中国科学院西安光学精密机械研究所 Two-dimensional optical phased array grating lobe elimination and phase modulation method
CN109659705B (en) * 2018-10-24 2022-07-29 纵目科技(上海)股份有限公司 MIMO radar two-dimensional sparse antenna array method, radar antenna, radar and storage medium
CA3148129A1 (en) * 2019-07-22 2021-01-28 Huawei Technologies Co., Ltd. Radar system and vehicle
CN111175703B (en) * 2019-12-31 2022-04-01 福瑞泰克智能系统有限公司 Antenna wave transmitting method and antenna arrangement
CN111505597B (en) * 2020-04-24 2023-04-14 南京市德赛西威汽车电子有限公司 Method for eliminating radar beam forming grating lobe and antenna
CN112731411B (en) * 2020-12-18 2022-08-23 之江实验室 Method for improving angular resolution of MIMO area array radar
CN113690590B (en) * 2021-08-23 2023-07-18 安徽大学 Multiple-input multiple-output sparse antenna
CN114879138B (en) * 2022-07-13 2022-09-27 广东大湾区空天信息研究院 Millimeter wave radar two-dimensional angle calculation method and device and related equipment
CN115296042A (en) * 2022-07-27 2022-11-04 重庆大学 Two-dimensional MIMO array arrangement method

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101666879A (en) * 2008-09-03 2010-03-10 电子科技大学 Method for improving resolution of linear-array three-dimensional imaging synthetic aperture radars
CN101950851A (en) * 2010-06-23 2011-01-19 电子科技大学 Staggered MIMO radar array antenna construction method

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6608584B1 (en) * 2002-02-12 2003-08-19 Raytheon Company System and method for bistatic SAR image generation with phase compensation

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101666879A (en) * 2008-09-03 2010-03-10 电子科技大学 Method for improving resolution of linear-array three-dimensional imaging synthetic aperture radars
CN101950851A (en) * 2010-06-23 2011-01-19 电子科技大学 Staggered MIMO radar array antenna construction method

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
《双基地SAR与线阵SAR原理及成像技术研究》;师君;《中国博士学位论文全文数据库》;20091130(第11期);第1-195页 *
Gao Xiang,Xiaoling Zhang,Jun Shi.《AIRBORNE 3-D FORWARD LOOKING SAR IMAGING VIA CHIRP SCALING ALGORITHM》.《Geoscience and Remote Sensing Symposium(IGARSS),2011 IEEE International》.2011,第3011-3014页. *
师君.《双基地SAR与线阵SAR原理及成像技术研究》.《中国博士学位论文全文数据库》.2009,(第11期),第1-195页.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3522300A1 (en) * 2018-02-05 2019-08-07 The Boeing Company Axisymmetric thinned digital beamforming array for reduced power consumption

Also Published As

Publication number Publication date
CN102521472A (en) 2012-06-27

Similar Documents

Publication Publication Date Title
CN102521472B (en) Method for constructing thinned MIMO (Multiple Input Multiple Output) planar array radar antenna
CN107526063B (en) Radar apparatus and method of processing radar signals
US20180166794A1 (en) 2d-mimo radar antenna array geometry and design method
US10446938B1 (en) Radar system including dual receive array
CN111656213B (en) Radar and antenna built in radar
CN105785328B (en) The decoupling Beamforming Method of FDA distance-angles based on Subarray partition
KR20180026470A (en) Angle and position detection using arrays of antennas
CN106772337B (en) A kind of two layers of dielectric object localization method of frequency diversity array based on MUSIC algorithm
CN104849696A (en) MIMO radar antenna array sparse arraying method
CN107576953A (en) Relevant and incoherent compound target DOA estimation method based on relatively prime MIMO array
CN108008388B (en) Satellite-borne phased array SAR load beam control method
CN102253363A (en) Device for estimating two-dimensional direction of arrival (DOA) of coherent signals based on L array and method thereof
CN103558594A (en) Phased array beamforming method based on airborne equipment
CN103412286B (en) Transmitting polarization optimizing DOA (direction of arrival) evaluation method based on MIMO (multiple-input multiple-output) radar
US20220326347A1 (en) Sparse antenna arrays for automotive radar
CN109765529B (en) Millimeter wave radar anti-interference method and system based on digital beam forming
CN112462363B (en) Non-uniform sparse polarization array coherent target parameter estimation method
CN102841335A (en) Iterative FFT-based quick MIMO radar waveform synthesis method
JP2024501521A (en) Radar equipment including multiple antennas spaced horizontally and vertically apart
CN110764059B (en) Method for transmitting and receiving vertical beam three-coordinate phased array radar
RU2682174C1 (en) Millimeter-range antenna array for the three-dimensional imaging radar system
CN104868946A (en) Adaptive weighted interference suppression method of subarray level mixed MIMO-phased array system
KR102163696B1 (en) Method for sending multiple beam steering jamming signal and system thereof
CN104808178B (en) A kind of airborne radar transmitting pattern method for designing
CN110320499A (en) MIMO radar beam transmitting beam pattern method based on Subarray partition

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130612