CN104569937B - A kind of new synthetic aperture radar corner reflector and its design method - Google Patents

A kind of new synthetic aperture radar corner reflector and its design method Download PDF

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CN104569937B
CN104569937B CN201510042788.7A CN201510042788A CN104569937B CN 104569937 B CN104569937 B CN 104569937B CN 201510042788 A CN201510042788 A CN 201510042788A CN 104569937 B CN104569937 B CN 104569937B
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mrow
msub
corner reflector
tau
mfrac
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CN104569937A (en
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李传荣
周勇胜
马灵玲
胡坚
唐伶俐
李子扬
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Academy of Opto Electronics of CAS
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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
    • 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
    • G01S7/40Means for monitoring or calibrating

Abstract

A kind of design method of new synthetic aperture radar corner reflector, comprises the following steps:Using input parameters such as radar system parameters, scaling requirements, trihedral corner reflector reflection plate suqare is calculated;According to reflecting plate boundary curve citation form, calculate area and be equal toCandidate edge curve form, that is,;According to candidateWithNumerical value pair, calculate corresponding minimum edge length;It is determined that the boundary curve of whole reflecting plate.The present invention is directed to conventional trihedral corner reflector corner ground clutter interference problem, and using the reflecting plate of full-reflector type, that is, all radar waves that corner reflector is exposed to along normal direction can return to radar after triple reflection;Secondly the problem of being also easy to produce reflecting plate edge diffraction for Low-frequency radar ripple, the reflection plate shape of optimization design trihedral corner reflector, so that the edge length of reflecting surface is most short in given reflection plate suqare lower edge length, so as to improve corner reflector applied to the calibration of SAR load and the precision of image quality measure.

Description

A kind of new synthetic aperture radar corner reflector and its design method
Technical field
The present invention relates to SAR remote sensing field, is related to a kind of new synthetic aperture radar corner reflector design side Method, it is that a kind of elimination corner reflector clutter influences and minimizes the new synthetic aperture radar corner reflection of reflecting plate edge length Device design method.The inventive method principle is simple, convenience of calculation, is commented available for synthetic aperture radar high accuracy Scaling with quality Valency.
Background technology
As the development of synthetic aperture radar (SAR) satellite remote sensing technology and the round-the-clock quantitative remote sensing application of round-the-clock need The continuous growth asked, in-orbit high accuracy Scaling is carried out to SAR, the importance of image quality evaluation becomes increasingly conspicuous.SAR is calibrated and figure Picture quality evaluation generally use corner reflector is carried out as point target, lays corner reflector at test site first, and it is anti-to obtain angle The SAR image of emitter;Corner reflector shows as " point " target with two-dimentional sinc function shapes in SAR image, in cross Shape, the resolution ratio of halfwidth (3dB pulsewidths) evaluation image of the main lobe power by calculating the point target;Reflected by trihedral angle The theoretical radar cross section (RCS) of device obtains radar cross section with measurement and determines calibration coefficient, and evaluation Electrodynamic radiation etc. is respectively Item quality index.
Trihedral corner reflector is the most widely used a kind of SAR corner reflectors.Trihedral corner reflector common at present is anti- Penetrating plate shape has isosceles right triangle, square, 1/4 circular arc etc..
Major technique defect:
(1) calibration of SAR load and image quality evaluation be by the theoretical RCS values of corner reflector and its in SAR image Brightness value contrasted so as to obtain calibration coefficient;Image is determined by the point target impulse response of corner reflector in the picture Quality index.In actual applications, corner reflector reflecting plate will produce " radar-earth's surface-trihedral angle reflection with background environment The Multiple Scattering effect of device-radar " or " radar-trihedral corner reflector-earth's surface-radar ".It is caused if ground is strong reflection face Extra RCS errors will be up to 16%.For high radiation calibration accuracy requirement, above-mentioned error is difficult to receive.
2) during corner reflector reflection radar wave, in reflecting plate marginal existence radar wave diffraction effect, this phenomenon pair Become apparent in Low-frequency radar ripple.The effect will make the RCS values that actually obtain and deviation occurs for theoretical RCS values, and then reduce SAR The precision of calibration and image quality evaluation.Edge diffraction is directly proportional to edge length, according to isoperimetric theorem, existing three face For the edge length of corner reflector under given reflection plate suqare, girth is not most short, thus can not optimally suppress edge around Penetrate the influence of effect.
The content of the invention
The present invention provides a kind of new synthetic aperture radar corner reflector and its design method, is made by the new design Ground clutter influence and edge diffraction influence can preferably be suppressed by obtaining corner reflector.
The present invention is directed to conventional trihedral corner reflector corner clutter problem, using the reflection of full-reflector reflector type Plate, that is, all radar waves for exposing to one reflecting plate of corner reflector can return to radar (no by another reflecting plate There is a situation where to return radar by ground return);Secondly the problem of being also easy to produce edge diffraction for Low-frequency radar ripple, optimization design The reflection plate shape of trihedral corner reflector so that the edge length of reflecting surface is most short in given reflection plate suqare lower edge length, So as to improve corner reflector applied to the calibration of SAR load and the precision of image quality measure.
It can be seen from the above technical proposal that the invention has the advantages that:
(1) as a result of full symmetrical configuration, corner reflector influenceed by Land-oceanic clutters it is small, to lay environment requirement it is low;
(2) edge length under equal corner reflector reflection plate suqare is smaller, RCS precision small by radar wave diffraction effect It is high;
(3) utilization rate of reflecting plate sheet material is high.
Brief description of the drawings
Fig. 1 is the flow chart of the inventive method;
Fig. 2 is corner reflector reflecting plate boundary curve general expression of the present invention;
Fig. 3 is C1For the reflecting plate schematic diagram of straight line;
Fig. 4 is C1For the reflecting plate schematic diagram of elliptic arc;
Fig. 5 is C1For the reflecting plate schematic diagram of circular arc;
Circular arc reflecting plate length of side L when Fig. 6 is different ribs long l;
Fig. 7 is the dimensional structure diagram using a kind of trihedral corner reflector of design method of the present invention design.
Embodiment
As shown in figure 1, the design method of the present invention comprises the following steps that:
A) using input parameters such as radar system parameters, scaling requirements, trihedral corner reflector reflection plate suqare A is calculated0
B) according to trihedral corner reflector reflecting plate basic configuration, calculate area and be equal to A0Candidate edge parameter of curve, That is, (y0,l)i
C) according to candidate y0With l numerical value to (y0,l)i, calculate corresponding trihedral corner reflector reflecting plate minimum edge length Spend Lmin
D the boundary curve parameter of whole reflecting plate) is determined.
Describe in detail as follows:
Step A:Inputted using radar system parameters (such as radar wavelength), scaling requirements (such as signal to noise ratio, calibration precision) Parameter, calculate trihedral corner reflector reflection plate suqare A0.It is to ensure the RCS of corner reflector to calculate trihedral corner reflector area Be worth sufficiently large so that it is guaranteed that corner reflector can be visible in radar image, at the same avoid corner reflection reflected intensity it is too high cause it is full With.
Wherein
S in formula1It is to meet the signal to noise ratio that given measuring uncertainty requires, such as S1During=14dB, measuring uncertainty is + 0.9dB arrives -0.8dB, works as S1During=20dB, measuring uncertainty is that+0.4dB arrives -0.4dB;S2For radar system dynamic range Higher limit, σ are corner reflector peak value RCS values, ρaAnd ρrIt is SAR load orientation and distance to resolution ratio;λ is radar center ripple It is long;σ0For ground backscattering coefficient.For the corner reflector for airborne synthetic aperture radar calibration and quality evaluation, take full The larger A of sufficient formula (1)0Value.
Step B:According to reflecting plate boundary curve citation form, as shown in figure 1, by a kind of traversal mode, calculating is appeared Product is equal to A0All candidate edge curve forms.Comprise the steps of:
B1, selection reflecting plate curve C1Curve form:
If selecting straight line, it is easy to develop processing as shown in figure 3, advantage is that structure is relatively easy, but same area can not be obtained Under shorter edge length, expression formula is
If selecting elliptic arc, it is not easy to develop processing as shown in figure 4, advantage is that structure is relative complex, but can obtain coplanar Shorter edge length under product, expression formula are
If circular arc is selected, as shown in figure 5, advantage and disadvantage, between above two shape, expression formula is
B2, according to selected reflecting plate basic configuration and corresponding boundary curve C1Expression formula, y is traveled through by one kind0 With l value methods, the reflection plate suqare A under respective value is calculated respectivelyc
Ac=2 ∫ (f1′g1-g′1f1)dτ (5)
In formula ' represent derivative.
B3, the candidate y for meeting to require according to formula (6) determination0With l values:
|Ac-A0| < e (6)
E represents threshold value, value 0.0001 in formula.
Step C:According to candidate y0With l numerical value pair, corresponding minimum edge length is calculated, is comprised the steps of:
C1, each y calculated according to following formula0With reflecting plate the edge length L, edge length L of l numerical value pairiWith liRelation such as Shown in Fig. 6.
C2, the L from calculatingiIn obtain minimum value, then obtain corresponding y0With l numerical value, so as to be met the edge of requirement Curve C1
Step D:Curve C is determined according to formula (8)2, and then according to C1And C2The shape of whole reflecting plate is determined on Z=X mirror images Shape.
C2(τ)=[0, g1(τ),g1(τ)-f1(τ)] (8)
It is using a kind of dimensional structure diagram of trihedral corner reflector of above-mentioned design method design, bag referring to Fig. 7 Support 2 and three reflecting plates 1 are included, three reflecting plates 1 are provided with a right angle, and the right-angle side of three reflecting plates 1 is connected with each other composition Three faces right angle, it is connected with the top of support 2 below one of reflecting plate 1.The other parts at three edges of reflecting plate 1 are served as reasons Curve C1With curve C2The A1 parts of connecting line composition, and be made up of A1 parts with A2 parts two parts of diagonal mirror images.
S1 is 20dB, S2 45dB, ground backscattering coefficient 5dB/m2 in the embodiment;ρaAnd ρrFor 1m;λ is 5.5cm.According to formula (1), A0 is obtained as 0.9.Consideration takes into account development and edge length, selects basic configuration of the edge for circular arc, Such as formula (4), according to step B and C, it may be determined that l 0.8962m, as shown in Figure 7.Support 2 is prior art, and having to adjust Save the function in inclination angle and direction.

Claims (2)

1. a kind of design method of new synthetic aperture radar corner reflector, it is characterised in that comprise the following steps:
A, using radar system parameters, scaling requirements input parameter, trihedral corner reflector reflection plate suqare A is calculated0
B, according to trihedral corner reflector reflecting plate basic configuration, calculate area and be equal to A0Candidate edge parameter of curve, that is, (y0,l)i
C, according to candidate y0With l numerical value to (y0,l)i, calculate the minimum edge length of corresponding trihedral corner reflector reflecting plate Lmin
D, the boundary curve parameter of whole reflecting plate is determined;
Trihedral corner reflector reflection plate suqare A in described step A0Calculated according to formula (1):
Wherein
S in formula1It is the signal to noise ratio for meeting given measuring uncertainty requirement, works as S1During=14dB, measuring uncertainty is+0.9dB To -0.8dB;Work as S1During=20dB, measuring uncertainty is that+0.4dB arrives -0.4dB;S2For polarization sensitive synthetic aperture radar system dynamic model Place limit value, σ is corner reflector peak value RCS values, ρaAnd ρrIt is synthetic aperture radar orientation and distance to resolution ratio;λ is radar Centre wavelength;σ0For the backscattering coefficient on ground;It is anti-with the angle of quality evaluation for being calibrated for airborne synthetic aperture radar Emitter, take the larger A for meeting formula (1)0Value;
Described step B:According to reflecting plate boundary curve citation form, by a kind of traversal mode, calculate area and be equal to A0's All candidate edge curve forms, are comprised the steps of:
B1, selection trihedral corner reflector reflecting plate basic configuration, that is, determine its boundary curve C1Form:
If selecting straight line, expression formula is:
<mrow> <mfenced open = "{" close = ""> <mtable> <mtr> <mtd> <mrow> <mi>y</mi> <mo>=</mo> <msub> <mi>f</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>&amp;tau;</mi> <mo>)</mo> </mrow> <mo>=</mo> <msub> <mi>y</mi> <mn>0</mn> </msub> <mo>+</mo> <mi>&amp;tau;</mi> </mrow> </mtd> </mtr> <mtr> <mtd> <mrow> <mi>z</mi> <mo>=</mo> <msub> <mi>g</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>&amp;tau;</mi> <mo>)</mo> </mrow> <mo>=</mo> <mn>2</mn> <msub> <mi>y</mi> <mn>0</mn> </msub> <mo>+</mo> <mfrac> <mrow> <mn>2</mn> <msub> <mi>y</mi> <mn>0</mn> </msub> <mo>-</mo> <mi>l</mi> </mrow> <msub> <mi>y</mi> <mn>0</mn> </msub> </mfrac> <mi>&amp;tau;</mi> </mrow> </mtd> </mtr> </mtable> </mfenced> <mo>,</mo> <mi>&amp;tau;</mi> <mo>&amp;Element;</mo> <mo>&amp;lsqb;</mo> <mo>-</mo> <msub> <mi>y</mi> <mn>0</mn> </msub> <mo>,</mo> <mn>0</mn> <mo>&amp;rsqb;</mo> <mo>-</mo> <mo>-</mo> <mo>-</mo> <mrow> <mo>(</mo> <mn>2</mn> <mo>)</mo> </mrow> </mrow>
If selecting elliptic arc, expression formula is:
<mrow> <mfenced open = "{" close = ""> <mtable> <mtr> <mtd> <mrow> <mi>y</mi> <mo>=</mo> <msub> <mi>f</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>&amp;tau;</mi> <mo>)</mo> </mrow> <mo>=</mo> <msub> <mi>y</mi> <mn>0</mn> </msub> <mo>+</mo> <mi>b</mi> <mi> </mi> <mi>cos</mi> <mi>&amp;tau;</mi> </mrow> </mtd> </mtr> <mtr> <mtd> <mrow> <mi>z</mi> <mo>=</mo> <msub> <mi>g</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>&amp;tau;</mi> <mo>)</mo> </mrow> <mo>=</mo> <mrow> <mo>(</mo> <mrow> <mi>l</mi> <mo>-</mo> <mi>x</mi> </mrow> <mo>)</mo> </mrow> <mo>+</mo> <mi>a</mi> <mi> </mi> <mi>sin</mi> <mi>&amp;tau;</mi> </mrow> </mtd> </mtr> </mtable> </mfenced> <mo>,</mo> <mi>&amp;tau;</mi> <mo>&amp;Element;</mo> <mrow> <mo>&amp;lsqb;</mo> <mrow> <mfrac> <mi>&amp;pi;</mi> <mn>2</mn> </mfrac> <mo>+</mo> <mi>arctan</mi> <mrow> <mo>(</mo> <mfrac> <msub> <mi>y</mi> <mn>0</mn> </msub> <mi>x</mi> </mfrac> <mo>)</mo> </mrow> <mo>,</mo> <mfrac> <mi>&amp;pi;</mi> <mn>2</mn> </mfrac> </mrow> <mo>&amp;rsqb;</mo> </mrow> <mo>-</mo> <mo>-</mo> <mo>-</mo> <mrow> <mo>(</mo> <mn>3</mn> <mo>)</mo> </mrow> </mrow>
If selecting circular arc, expression formula is:
<mrow> <mfenced open = "{" close = ""> <mtable> <mtr> <mtd> <mrow> <mi>y</mi> <mo>=</mo> <msub> <mi>f</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>&amp;tau;</mi> <mo>)</mo> </mrow> <mo>=</mo> <msub> <mi>y</mi> <mn>0</mn> </msub> <mo>+</mo> <mi>r</mi> <mi> </mi> <mi>cos</mi> <mi>&amp;tau;</mi> </mrow> </mtd> </mtr> <mtr> <mtd> <mrow> <mi>z</mi> <mo>=</mo> <msub> <mi>g</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>&amp;tau;</mi> <mo>)</mo> </mrow> <mo>=</mo> <mrow> <mo>(</mo> <mi>l</mi> <mo>-</mo> <mi>x</mi> <mo>)</mo> </mrow> <mo>+</mo> <mi>r</mi> <mi> </mi> <mi>sin</mi> <mi>&amp;tau;</mi> </mrow> </mtd> </mtr> </mtable> </mfenced> <mo>,</mo> <mi>&amp;tau;</mi> <mo>&amp;Element;</mo> <mo>&amp;lsqb;</mo> <mfrac> <mi>&amp;pi;</mi> <mn>2</mn> </mfrac> <mo>+</mo> <mi>arctan</mi> <mrow> <mo>(</mo> <mfrac> <msub> <mi>y</mi> <mn>0</mn> </msub> <mi>x</mi> </mfrac> <mo>)</mo> </mrow> <mo>,</mo> <mfrac> <mi>&amp;pi;</mi> <mn>2</mn> </mfrac> <mo>&amp;rsqb;</mo> <mo>-</mo> <mo>-</mo> <mo>-</mo> <mrow> <mo>(</mo> <mn>4</mn> <mo>)</mo> </mrow> </mrow>
B2, according to selected reflecting plate basic configuration and corresponding boundary curve C1Expression formula, y is traveled through by one kind0And l Value method, calculate corresponding reflection plate suqare Ac
Ac=2 ∫ (f1′g1-g1′f1)dτ (5)
In formula ' represent derivative;
B3, the candidate y for meeting to require according to formula (6) determination0With l values:
|Ac-A0| < e (6)
E represents threshold value, value 0.0001 in formula;
Described step C:According to candidate y0With l numerical value pair, corresponding minimum edge length is calculated, is comprised the steps of:
C1, each y calculated according to following formula0With reflecting plate the edge length L, edge length L of l numerical value pairiWith liRelational expression be:
<mrow> <msub> <mi>L</mi> <mi>i</mi> </msub> <mo>=</mo> <mn>2</mn> <mo>&amp;CenterDot;</mo> <mo>&amp;Integral;</mo> <mo>{</mo> <msqrt> <mrow> <msubsup> <mi>f</mi> <mrow> <mn>1</mn> <mi>i</mi> </mrow> <mrow> <mo>&amp;prime;</mo> <mn>2</mn> </mrow> </msubsup> <mo>+</mo> <msubsup> <mi>g</mi> <mrow> <mn>1</mn> <mi>i</mi> </mrow> <mrow> <mo>&amp;prime;</mo> <mn>2</mn> </mrow> </msubsup> </mrow> </msqrt> <mo>+</mo> <msqrt> <mrow> <msup> <mrow> <mo>(</mo> <msubsup> <mi>f</mi> <mrow> <mn>1</mn> <mi>i</mi> </mrow> <mo>&amp;prime;</mo> </msubsup> <mo>-</mo> <msubsup> <mi>g</mi> <mrow> <mn>1</mn> <mi>i</mi> </mrow> <mo>&amp;prime;</mo> </msubsup> <mo>)</mo> </mrow> <mn>2</mn> </msup> <mo>+</mo> <msubsup> <mi>g</mi> <mrow> <mn>1</mn> <mi>i</mi> </mrow> <mrow> <mo>&amp;prime;</mo> <mn>2</mn> </mrow> </msubsup> </mrow> </msqrt> <mo>}</mo> <mi>d</mi> <mi>&amp;tau;</mi> <mo>-</mo> <mo>-</mo> <mo>-</mo> <mrow> <mo>(</mo> <mn>7</mn> <mo>)</mo> </mrow> </mrow>
C2, the L from calculatingiIn obtain minimum value, then obtain corresponding y0With l numerical value, so as to be met the boundary curve of requirement C1
Described step D:Curve C is determined according to formula (8)2
C2(τ)=[0, g1(τ),g1(τ)-f1(τ)] (8)
And then according to C1And C2The shape of whole reflecting plate is determined on Z=X mirror images.
A kind of 2. new synthetic aperture radar corner reflector that design method using described in claim 1 designs.
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Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105301570B (en) * 2015-10-20 2017-07-14 中国科学院电子学研究所 A kind of outfield calibration method of airborne straight rail interference SAR system
CN105629208B (en) * 2016-01-08 2018-09-18 中国人民解放军国防科学技术大学 A kind of synthetic aperture radar two dimensional image modulator based on phase-modulation surface
CN108594191B (en) * 2018-04-24 2020-03-17 北京环境特性研究所 Three-sided corner reflector, method and device for determining semi-elliptical concave structure
CN109459736B (en) * 2019-01-04 2020-10-13 北京环境特性研究所 Radar target design method and device
CN110118968B (en) * 2019-04-30 2021-01-05 华中科技大学 Inclined four-reflecting-plate mirror image synthetic aperture radiometer and imaging method
CN112444783A (en) * 2019-09-05 2021-03-05 中国科学院光电研究院 Synthetic aperture radar on-orbit rapid calibration method based on natural uniform target

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102401892A (en) * 2010-09-19 2012-04-04 中国科学院电子学研究所 System performance assessment method of polarized interferometric synthetic aperture radar
CN102608601A (en) * 2012-03-08 2012-07-25 北京北科安地科技发展有限公司 Method for recognizing artificial corner reflector in SAR (synthetic aperture radar) image
CN103091666A (en) * 2011-11-07 2013-05-08 中国科学院电子学研究所 Onboard P-waveband polarization synthetic aperture radar (SAR) calibration method under non-ideal calibrator condition

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2001091649A (en) * 1999-09-20 2001-04-06 Mitsubishi Electric Corp Ground control point device for synthetic aperture radar image precise geometrical correction

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102401892A (en) * 2010-09-19 2012-04-04 中国科学院电子学研究所 System performance assessment method of polarized interferometric synthetic aperture radar
CN103091666A (en) * 2011-11-07 2013-05-08 中国科学院电子学研究所 Onboard P-waveband polarization synthetic aperture radar (SAR) calibration method under non-ideal calibrator condition
CN102608601A (en) * 2012-03-08 2012-07-25 北京北科安地科技发展有限公司 Method for recognizing artificial corner reflector in SAR (synthetic aperture radar) image

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
"Analysis of Radar Cross Sectional Area of Corner Reflectors";Tarig Ibrahim Osman,等;《IOSR Journal of Engineering》;20141231;第04卷;第47-51页 *
"IMPROVED TRIHEDRAL CORNER REFLECTOR FOR HIGH-PRECISION SAR CALIBRATION AND VALIDATION";Yongsheng Zhou,等;《2014 IEEE Geosicence and Remote Sensing Symposium》;20140718;第455页第1节第2-3段、第2节,第456页第3节1-4段及图2-4、图6 *
"Optimum Corner Reflectors for Calibration of Imaging Radars";Kamal Sarabandi,等;《IEEE TRANSACTIONS ON ANTENNAS AND PROPAGATION》;19961030;第44卷(第10期);第1349页第II部分B中第1段、第1352页第D部分第1段 *

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