CN111180894A - OAM antenna dark space reduction method based on frequency selection surface - Google Patents

OAM antenna dark space reduction method based on frequency selection surface Download PDF

Info

Publication number
CN111180894A
CN111180894A CN201911363935.5A CN201911363935A CN111180894A CN 111180894 A CN111180894 A CN 111180894A CN 201911363935 A CN201911363935 A CN 201911363935A CN 111180894 A CN111180894 A CN 111180894A
Authority
CN
China
Prior art keywords
antenna
oam
frequency
frequency selective
selective surface
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.)
Granted
Application number
CN201911363935.5A
Other languages
Chinese (zh)
Other versions
CN111180894B (en
Inventor
胡俊
赵润哲
吴文
杨景
胡燕金
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.)
Nanjing University of Science and Technology
Original Assignee
Nanjing University of Science and Technology
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 Nanjing University of Science and Technology filed Critical Nanjing University of Science and Technology
Priority to CN201911363935.5A priority Critical patent/CN111180894B/en
Publication of CN111180894A publication Critical patent/CN111180894A/en
Application granted granted Critical
Publication of CN111180894B publication Critical patent/CN111180894B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/0006Devices acting selectively as reflecting surface, as diffracting or as refracting device, e.g. frequency filtering or angular spatial filtering devices
    • H01Q15/0013Devices acting selectively as reflecting surface, as diffracting or as refracting device, e.g. frequency filtering or angular spatial filtering devices said selective devices working as frequency-selective reflecting surfaces, e.g. FSS, dichroic plates, surfaces being partly transmissive and reflective
    • H01Q15/0046Theoretical analysis and design methods of such selective devices

Abstract

The invention discloses an OAM antenna dark space reduction method based on a frequency selection surface, which loads a two-dimensional band-pass frequency selection surface above an OAM antenna to improve the far-field characteristic of the antenna; when electromagnetic waves are incident, the angle stability of the frequency selective surface enables the non-uniform plane wave components of the OAM waves in all directions to be filtered; the method can change the far-field characteristics of the antenna, such as bandwidth, gain and the like, while reshaping the OAM waveform, and the characteristics can be changed by adjusting the geometric structure, the arrangement mode and the physical parameters of the frequency selection surface. The invention designs the adjusting scheme of each parameter by analyzing the influence of each parameter of the frequency selection surface on the characteristics, and finally obtains the high-gain antenna with obviously reduced dark area.

Description

OAM antenna dark space reduction method based on frequency selection surface
Technical Field
The invention relates to the technical field of wireless communication, in particular to an OAM antenna dark space reduction method based on a frequency selective surface.
Background
With the advent of the high-speed information age, the development of the high-frequency band millimeter wave communication technology can greatly alleviate the shortage of frequency spectrum. At present, technologies such as Code Division Multiplexing (CDM), Time Division Multiplexing (TDM), polarization multiplexing (PDM), Orthogonal Frequency Division Multiplexing (OFDM), and Multiple Input Multiple Output (MIMO) have been applied to solve the problem of spectrum resource shortage, but the application of these technologies still has difficulty in meeting the development trend of higher speed and higher bandwidth for future communication. Therefore, it is becoming a trend to find other multiplexing techniques with new dimensions to improve the spectrum utilization.
Orbital Angular Momentum (OAM) can be used as a new modulation scheme in radio communication systems. The OAM vortex electromagnetic wave carrying information can be transmitted in parallel in the same bandwidth by the OAM multiplexing-based communication technology, and the utilization rate of frequency spectrum can be greatly improved. OAM has been widely used in optics, and by introducing OAM, transmission capability of an optical communication system is greatly improved. The new modulation technique OAM is applied in the microwave band, which presupposes that a high quality OAM beam can be obtained. Therefore, exploring and designing the high-gain OAM antenna with a small dark area has important significance for the practical application of the OAM technology in the microwave radio frequency field.
Since the OAM beam is hollow, the field strength of the middle area, i.e. the dark area, is weak, and as the propagation distance increases, the dark area becomes larger, which makes how to receive the OAM wave a difficult problem. The current methods for receiving the OAM wave include the following methods: the two-point method and the phase gradient method are convenient in single OAM mode receiving detection, but cannot be used in multiple OAM mode receiving; the Partial Angular Aperture Reception (PAAR) method and the Partial Aperture Sampling Reception (PASR) method cannot effectively calculate the OAM mode spectrum utilization; with the variable-scale aperture sampling reception (VSASR) method, orthogonality is slightly impaired, and there are also some other modes of crosstalk OAM.
Disclosure of Invention
The invention aims to provide a frequency selective surface-based OAM antenna dark area reduction method.
The technical solution for realizing the purpose of the invention is as follows: a OAM antenna dark space reduction method based on a frequency selective surface comprises the following steps:
s1, designing a single-layer single-side band-pass frequency selection surface, wherein the overall size of the single-layer single-side band-pass frequency selection surface is equal to the size of an antenna ground plane, and the passband bandwidth of the single-layer single-side band-pass frequency selection surface covers the passband bandwidth of the OAM antenna;
s2, loading the frequency selection surface on the OAM antenna, and setting the distance between the FSS and the OAM antenna according to the Fabry-Perot resonant cavity theory;
s3, changing the dielectric constant of the frequency selective surface substrate, establishing a concave function curve of the frequency selective surface substrate and the OAM antenna non-zero mode dark area, and finding the lowest point of the concave function curve, namely the minimum point of the antenna dark area;
s4, deriving a relation formula y of 0.054+0.046 sin (pi (x +0.74)/3.85) according to the thickness of the dielectric substrate on the frequency selective surface and the frequency deviation curve of the incident angle, where x is the thickness of the dielectric substrate on the frequency selective surface, and y is the deviation difference of the central frequency at the incident angle of 60 ° relative to the central frequency at the incident angle of 0 °, so that the central frequency deviation is minimized at the incident angle of 60 °, i.e. the angle stability is optimized.
Compared with the prior art, the invention has the following remarkable advantages: (1) the fundamental reason for the defects of the traditional receiving method is that the OAM wave with serious wave beam divergence phenomenon can not be completely received, but the method provided by the invention can reduce the divergence angle, namely reduce the area of a dark area, so that the complete receiving of the OAM wave becomes possible; (2) the method for reducing the dark area combines the OAM antenna with the frequency selection surface, and different frequency selection surfaces can be loaded according to the practical application requirement of the OAM antenna, so that the method has the advantages that the characteristics of high gain and small dark area can be kept all the time; (3) the method has strong practicability for receiving the OAM wave and improving the antenna transmission quality.
Drawings
Fig. 1 is a flow chart of the OAM antenna dark space reduction method based on the frequency selective surface of the present invention.
Fig. 2 is a diagram of an antenna structure in the embodiment of the present invention.
FIG. 3 is a graph of the concave function between the dielectric constant and the 0db dark point for an embodiment of the present invention.
FIG. 4 is a data result diagram of unloaded FSS and loaded FSS according to an embodiment of the present invention.
Detailed Description
Aiming at the hollow vortex characteristic of an OAM wave beam, the invention provides a method for reducing the dark area of an OAM antenna based on a frequency selection surface, wherein the frequency selection surface is loaded above the OAM antenna and comprises an antenna main body and the frequency selection surface; the antenna main body is used for transmitting OAM waves, and the frequency selection surface is loaded on the antenna main body and used for carrying out spatial filtering on the OAM antenna.
As shown in fig. 1, the method comprises the steps of:
s1, designing a single-layer single-side band-pass frequency selection surface, wherein the whole size of the single-layer single-side band-pass frequency selection surface is equal to the size of an antenna ground plane, and the passband bandwidth of the single-layer single-side band-pass frequency selection surface covers the passband bandwidth of the OAM antenna;
s2, loading the frequency selection surface on the OAM antenna, and setting the distance between the FSS and the OAM antenna according to the Fabry-Perot resonant cavity theory;
s3, changing the dielectric constant of the frequency selective surface substrate, establishing a concave function curve of the frequency selective surface substrate and the OAM antenna non-zero mode dark area, and finding the lowest point of the concave function curve, namely the minimum point of the antenna dark area;
and S4, deriving a relation formula y of 0.054+0.046 sin (pi (x +0.74)/3.85) according to the thickness of the dielectric substrate on the frequency selection surface and the frequency deviation curve of the incident angle, wherein x is the thickness of the dielectric substrate on the frequency selection surface, and y is the deviation difference of the central frequency at the incident angle of 60 degrees relative to the central frequency at the incident angle of 0 degrees. The central frequency deviation is minimized when the incidence angle is 60 degrees, namely, the angle stability is optimized.
Further, step S1 specifically includes:
designing a unit cell, etching a pattern on a metal surface of the unit cell, and setting a simulation boundary condition as a cell boundary condition;
through mathematical calculation and simulation optimization of the existing mature technology, when plane waves enter the two-dimensional periodic structure which is infinitely and uniformly distributed, the passband bandwidth of the two-dimensional periodic structure covers the passband bandwidth of the OAM antenna;
according to the actual size of the OAM antenna, a single-layer single-face band-pass frequency selection surface with limited-size units periodically arranged along the X axis, the Y axis and the like is finally formed by combining the designed unit units.
Further, step S2 specifically includes:
loading a frequency selection surface above the OAM antenna, so that the frequency selection surface and an antenna ground plate form a Fabry-Perot resonant cavity;
and according to a Fabry-Perot cavity antenna theoretical formula, setting the distance between the FSS and the antenna to ensure that the cavity height meets the resonance condition, and further ensuring that the axial direction of the antenna has the maximum radiation direction.
Further, step S3 specifically includes:
and changing the dielectric constant of the frequency selective surface substrate to establish a concave function curve of the frequency selective surface substrate and the non-zero mode dark region of the OAM antenna.
According to the relationship curve between the two, it can be found that the OAM beam dark area can be significantly changed by changing the dielectric constant, and the dielectric constant corresponding to the lowest point of the curve is found, and the corresponding dark area is the minimum dark area.
Furthermore, OAM waves are emitted through the antenna main body, signals transmitted by the antenna main body are subjected to spatial filtering through the frequency selective surface, and finally the high-gain antenna with the obviously reduced dark area is obtained.
Further, the frequency selective surface includes a metal patch portion and a dielectric substrate: the metal patch part is connected with the dielectric substrate; and by changing various parameters of the dielectric substrate and the metal patch part, especially the dielectric constant, the high-gain antenna with the obviously reduced OAM wave beam dark area can be obtained. At present, no calculation research on the area of a dark area exists at home and abroad, but the reduction of the dark area is directly reflected by the reduction of divergence. The result of the examples below is a reduction in divergence angle to half that when the FSS is not loaded.
Furthermore, the frequency selective surface is a spatial band-pass filter, signals output from the antenna main body are designed and filtered according to the frequency band where the signals are located through the band-pass filter, and the pass band and the stop band of the band-pass filter are set according to the frequency band where the signals output by the antenna main body are located.
In consideration of the oblique incident wave characteristic of the OAM antenna, the dielectric substrate should be thick enough so that the frequency selective surface has good angular stability.
The invention will be further explained and supplemented with reference to the following examples.
Examples
As shown in fig. 2, the present embodiment provides an antenna for realizing dark space reduction of an OAM beam, the antenna including an antenna body, a frequency selective surface; the antenna body is used for transmitting OAM wave beams; the frequency selective surface is loaded above the antenna body and is used for carrying out spatial filtering on OAM waves.
In the embodiment shown in fig. 2, the antenna body includes a dielectric substrate 1, a dielectric substrate 2, a radiating patch 3, and a ground substrate 4. The upper surface of the dielectric substrate 2 is printed with a rectangular radiation patch 3, the lower surface of the dielectric substrate 2 is printed with a square grounding substrate 4, and the dielectric substrate 1 is printed on the lower surface of the grounding substrate 4. The feeding mode adopts coaxial feeding, four feeding ports are arranged below the dielectric substrate 1, the dielectric substrates 1 and 2 and the grounding substrate 4 are provided with through holes, an inner conductor of a coaxial connector penetrates through the through holes to be welded with the radiation patch 3, and an outer conductor is connected with the grounding substrate 4 to form a bottom feeding structure.
In the embodiment shown in fig. 2, the frequency selective surface includes a dielectric substrate 5 and a metal patch part 6, and the surface of the FSS is formed by a plurality of metal patch units 6 arranged periodically. The surface is a band-pass frequency selection surface, and the pass band and the stop band of the surface are designed according to the frequency band of the OAM wave transmitted by the antenna main body, so that the frequency band of the signal output by the output port is consistent with the frequency band of the signal originally output by the output port, and clutter is filtered.
As shown in fig. 1, the dark space reduction method based on the frequency selective surface of the present invention comprises the following steps:
s1, designing a single-layer single-side band-pass frequency selection surface, wherein the size of the single-layer single-side band-pass frequency selection surface is equal to the size of an antenna ground plane, and the passband bandwidth of the single-layer single-side band-pass frequency selection surface covers the passband bandwidth of the OAM antenna, and the method specifically comprises the following steps:
A. designing a unit cell, etching a pattern on the metal surface, and setting the simulation boundary condition as the cell boundary condition.
B. Through mathematical calculation and simulation optimization, the two-dimensional periodic structure which is infinitely and uniformly distributed can reach the purpose that the passband bandwidth covers the passband bandwidth of the OAM antenna when plane waves enter.
C. According to the actual size of the OAM antenna, a single-layer single-face band-pass frequency selection surface with limited-size units periodically arranged along the X axis, the Y axis and the like is finally formed by combining the designed unit units.
In the embodiment, the frequency selective surface loaded by the annular gap is selected, and the distance between the unit and the annular gap of the unit is ensured to be small enough to prevent the premature occurrence of grating lobes. The perimeter of the designed annular slot is approximately equal to the wavelength of the resonant frequency of the antenna.
S2, loading the frequency selection surface on the OAM antenna, and setting the distance between the FSS and the OAM antenna according to the Fabry-Perot resonant cavity theory, which specifically comprises the following steps:
A. and loading a frequency selection surface above the OAM antenna, so that the frequency selection surface and the antenna ground plate form a Fabry-Perot resonant cavity.
B. And according to a Fabry-Perot cavity antenna theoretical formula, setting the distance between the FSS and the antenna to ensure that the cavity height meets the resonance condition, and further ensuring that the axial direction of the antenna has the maximum radiation direction.
In the step B, when the height of the cavity meets the resonance condition, one part of the electromagnetic waves radiated by the OAM antenna is transmitted outwards through the FSS, the other part of the electromagnetic waves is reflected back into the resonant cavity, and the electromagnetic waves after multiple reflections are superposed on the outer surface of the FSS in the same phase to form high-gain radiation, so that the directivity of the antenna is improved, and the beam width is sharpened.
S3, changing the dielectric constant of the frequency selective surface substrate, establishing a concave function curve of the frequency selective surface substrate and the OAM antenna non-zero mode dark area, and finding the lowest point of the concave function curve, namely the minimum point of the dark area.
When the dielectric constant of the frequency selective surface substrate is changed, the beam pointing direction of the main lobe is gradually biased to normal phase while the dark area is reduced. When the dielectric constant increases to the increasing region of the relationship curve, it is found that the main beam pointing direction gradually deviates from the normal phase while the dark region is enlarged.
And changing the dielectric constant of the frequency selective surface substrate to establish a concave function curve of the frequency selective surface substrate and the non-zero mode dark region of the OAM antenna. The graph of this embodiment is shown in fig. 3, and it can be clearly seen that the function graph is a concave function curve, and the 0db angle in the dark region is the minimum when the dielectric constant is 3.5, which is the minimum point in the dark region.
S4, deriving a relation formula y of 0.054+0.046 sin (pi (x +0.74)/3.85) according to the frequency-selective surface dielectric substrate thickness and incident angle frequency deviation curve, so that the central frequency deviation is minimum at an incident angle of 60 °, that is, the angle stability is optimal.
When the thickness of the dielectric substrate of the frequency selective surface is changed, it can be found that the angular stability of the frequency selective surface is significantly improved. Due to the oblique incident wave characteristic of the uniform circular array OAM antenna of the embodiment, the angular stability of the frequency selective surface is very important.
In the embodiment of the dark area reduction method based on the frequency selective surface of the present invention, compared with the result of not loading the frequency selective surface, the angle of the dark area is reduced to half of the original angle at the directional diagram 0db, and the data is summarized as shown in fig. 4. The method provides possibility for receiving most of OAM wave at long distance and even completely receiving OAM wave.

Claims (7)

1. A OAM antenna dark space reduction method based on a frequency selective surface is characterized by comprising the following steps:
s1, designing a single-layer single-side band-pass frequency selection surface, wherein the overall size of the single-layer single-side band-pass frequency selection surface is equal to the size of an antenna ground plane, and the passband bandwidth of the single-layer single-side band-pass frequency selection surface covers the passband bandwidth of the OAM antenna;
s2, loading the frequency selection surface on the OAM antenna, and setting the distance between the FSS and the OAM antenna according to the Fabry-Perot resonant cavity theory;
s3, changing the dielectric constant of the frequency selective surface substrate, establishing a concave function curve of the frequency selective surface substrate and the OAM antenna non-zero mode dark area, and finding the lowest point of the concave function curve, namely the minimum point of the antenna dark area;
s4, deriving a relation formula y of 0.054+0.046 sin (pi (x +0.74)/3.85) according to the thickness of the dielectric substrate on the frequency selective surface and the frequency deviation curve of the incident angle, where x is the thickness of the dielectric substrate on the frequency selective surface, and y is the deviation difference of the central frequency at the incident angle of 60 ° relative to the central frequency at the incident angle of 0 °, so that the central frequency deviation is minimized at the incident angle of 60 °, i.e. the angle stability is optimized.
2. The method according to claim 1, wherein the step S1 specifically comprises:
designing a unit cell, etching a pattern on a metal surface of the unit cell, and setting a simulation boundary condition as a cell boundary condition;
through mathematical calculation and simulation optimization, when plane waves enter the two-dimensional periodic structure which is infinitely and uniformly distributed, the passband bandwidth of the two-dimensional periodic structure covers the passband bandwidth of the OAM antenna;
according to the actual size of the OAM antenna, a single-layer single-side band-pass frequency selection surface with units of limited size periodically arranged along the X axis, the Y axis and the like is formed by combining the designed unit units.
3. The method according to claim 1, wherein the step S2 specifically comprises:
loading a frequency selection surface above the OAM antenna, so that the frequency selection surface and an antenna ground plate form a Fabry-Perot resonant cavity;
and according to a Fabry-Perot cavity antenna theoretical formula, setting the distance between the FSS and the antenna to ensure that the cavity height meets the resonance condition and the axial direction of the antenna has the maximum radiation direction.
4. The method according to claim 1, wherein the step S3 specifically comprises:
changing the dielectric constant of the frequency selective surface substrate, and establishing a concave function curve of the frequency selective surface substrate and the non-zero mode dark region of the OAM antenna;
and finding out the dielectric constant corresponding to the lowest point of the curve according to the relation curve between the two, wherein the corresponding dark area is the minimum dark area.
5. The frequency selective surface based OAM antenna dark space reduction method of claim 1, wherein the OAM waves are transmitted through an antenna body, and signals transmitted by said antenna body are spatially filtered through the frequency selective surface.
6. The frequency selective surface based OAM antenna dark space reduction method of claim 1 or 5, wherein the frequency selective surface comprises a metal patch part and a dielectric substrate, the metal patch part being connected with the dielectric substrate.
7. The method of claim 1 or 5, wherein the frequency selective surface based OAM antenna dark space reduction is a spatial band pass filter.
CN201911363935.5A 2019-12-26 2019-12-26 OAM antenna dark space reduction method based on frequency selection surface Active CN111180894B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911363935.5A CN111180894B (en) 2019-12-26 2019-12-26 OAM antenna dark space reduction method based on frequency selection surface

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911363935.5A CN111180894B (en) 2019-12-26 2019-12-26 OAM antenna dark space reduction method based on frequency selection surface

Publications (2)

Publication Number Publication Date
CN111180894A true CN111180894A (en) 2020-05-19
CN111180894B CN111180894B (en) 2021-06-04

Family

ID=70648953

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201911363935.5A Active CN111180894B (en) 2019-12-26 2019-12-26 OAM antenna dark space reduction method based on frequency selection surface

Country Status (1)

Country Link
CN (1) CN111180894B (en)

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102723541A (en) * 2012-06-14 2012-10-10 北京航空航天大学 Method for optimizing cross-shaped annular slot frequency selection surface unit structural body and conformal antenna housing with low radar cross-section (RCS)
CN103985969A (en) * 2014-05-26 2014-08-13 西安电子科技大学 Method for designing dielectric reflector antenna
WO2015001410A1 (en) * 2013-07-01 2015-01-08 Matteoni Marco Celso System for generation and management of orbital angular momentum in electromagnetic radiation by means of special lens
CN105552556A (en) * 2015-12-28 2016-05-04 西安电子科技大学 Orbital angular momentum vortex wave beam generation apparatus and method
CN105826692A (en) * 2016-05-26 2016-08-03 哈尔滨工业大学 Lens and method for generating vortex beam with convergence effect based on super surface
CN106299674A (en) * 2016-08-17 2017-01-04 大连理工大学 A kind of frequency-selective surfaces antenna house bandwidth compensation method
CN107093801A (en) * 2017-05-02 2017-08-25 西安电子科技大学 High-gain orbital angular momentum array antenna based on the super surface of individual layer electromagnetism
CN206471491U (en) * 2016-10-31 2017-09-05 宁夏大学 A kind of multi-modal OAM electromagnetism vortex ripple array antenna of twin nuclei
CN108511919A (en) * 2018-02-06 2018-09-07 西安电子科技大学 A kind of converging device of vortex electromagnetic wave
CN108767496A (en) * 2018-05-31 2018-11-06 西安电子科技大学 The generating means of high-gain pencil beam and orbital angular momentum vortex wave beam
CN108767495A (en) * 2018-05-24 2018-11-06 西安电子科技大学 A kind of vortex electromagnetism wave generation device based on super surface
CN108963465A (en) * 2018-09-16 2018-12-07 复旦大学 A kind of honeycomb Meta Materials surface that can generate orbital angular momentum wave
CN108987939A (en) * 2018-08-14 2018-12-11 西安电子科技大学 A kind of converging device, the wireless communication system of vortex electromagnetic wave

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102723541A (en) * 2012-06-14 2012-10-10 北京航空航天大学 Method for optimizing cross-shaped annular slot frequency selection surface unit structural body and conformal antenna housing with low radar cross-section (RCS)
WO2015001410A1 (en) * 2013-07-01 2015-01-08 Matteoni Marco Celso System for generation and management of orbital angular momentum in electromagnetic radiation by means of special lens
CN103985969A (en) * 2014-05-26 2014-08-13 西安电子科技大学 Method for designing dielectric reflector antenna
CN105552556A (en) * 2015-12-28 2016-05-04 西安电子科技大学 Orbital angular momentum vortex wave beam generation apparatus and method
CN105826692A (en) * 2016-05-26 2016-08-03 哈尔滨工业大学 Lens and method for generating vortex beam with convergence effect based on super surface
CN106299674A (en) * 2016-08-17 2017-01-04 大连理工大学 A kind of frequency-selective surfaces antenna house bandwidth compensation method
CN206471491U (en) * 2016-10-31 2017-09-05 宁夏大学 A kind of multi-modal OAM electromagnetism vortex ripple array antenna of twin nuclei
CN107093801A (en) * 2017-05-02 2017-08-25 西安电子科技大学 High-gain orbital angular momentum array antenna based on the super surface of individual layer electromagnetism
CN108511919A (en) * 2018-02-06 2018-09-07 西安电子科技大学 A kind of converging device of vortex electromagnetic wave
CN108767495A (en) * 2018-05-24 2018-11-06 西安电子科技大学 A kind of vortex electromagnetism wave generation device based on super surface
CN108767496A (en) * 2018-05-31 2018-11-06 西安电子科技大学 The generating means of high-gain pencil beam and orbital angular momentum vortex wave beam
CN108987939A (en) * 2018-08-14 2018-12-11 西安电子科技大学 A kind of converging device, the wireless communication system of vortex electromagnetic wave
CN108963465A (en) * 2018-09-16 2018-12-07 复旦大学 A kind of honeycomb Meta Materials surface that can generate orbital angular momentum wave

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
徐豪骏: "可调超表面天线罩的设计与应用研究", 《中国优秀硕士学位论文全文数据库》 *

Also Published As

Publication number Publication date
CN111180894B (en) 2021-06-04

Similar Documents

Publication Publication Date Title
US6140972A (en) Multiport antenna
US20180226727A1 (en) Module, wireless communication apparatus, and radar apparatus
CN112886272B (en) Dual-frequency dual-polarization Fabry-Perot resonant cavity antenna
US6172654B1 (en) Conical omni-directional coverage multibeam antenna
KR20050109320A (en) Array spacing decision method at array antenna using genetic algorithm and array antenna with sofa structure and irregular array spacing
US20220311129A1 (en) Transmitting Antenna System, Receiving Antenna System and Communication Device
US10135156B2 (en) Multi-mode composite antenna
CN111052507B (en) Antenna and wireless device
CN113922075A (en) Slow wave substrate integrated waveguide duplex antenna based on high-order mode
CN113013638A (en) Broadband folding type plane reflection array antenna
CN110224232B (en) Antenna system and method for reducing signal radiation in undesired directions
CN107799888B (en) Dual-frequency high-gain patch antenna
CN111326853B (en) Near-field low-sidelobe flat-topped Bessel-Gauss beam radial slot array antenna
US10892562B1 (en) Multi-beam Yagi-based MIMO antenna system
CN111180894B (en) OAM antenna dark space reduction method based on frequency selection surface
WO2021003030A1 (en) Antenna feed networks and related antennas and methods
WO2020194188A2 (en) Frasera antenna radiator (far) for 5g array antennas
CN116093598A (en) Broadband dual-frequency transmission array unit, antenna and use method thereof
CN112397882B (en) Wide-beam high-gain ranging antenna for high-orbit satellite
Farahani et al. A Novel Planar Coupled-resonator Cavity-backed Slot Array Filtenna
Pedram et al. Evolution and move toward fifth-generation antenna
CN113690553B (en) Near-field microwave conversion device with adjustable wave beam
CN117335169B (en) Dual-frequency dual-circular polarization transmission array antenna and method for 5G millimeter wave system
CN216085339U (en) Omnidirectional annular slot array antenna
US20230261387A1 (en) Metasurface superstrate (mss) enabled radiator for a multiband antenna apparatus

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant