[go: up one dir, main page]

CN1652400A - Voltage control adaptive aerial - Google Patents

Voltage control adaptive aerial Download PDF

Info

Publication number
CN1652400A
CN1652400A CN 200510009754 CN200510009754A CN1652400A CN 1652400 A CN1652400 A CN 1652400A CN 200510009754 CN200510009754 CN 200510009754 CN 200510009754 A CN200510009754 A CN 200510009754A CN 1652400 A CN1652400 A CN 1652400A
Authority
CN
China
Prior art keywords
antenna
fixed
dielectric layer
layer body
variable dielectric
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
CN 200510009754
Other languages
Chinese (zh)
Other versions
CN100355149C (en
Inventor
沙学军
顾学迈
张中兆
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.)
Harbin Institute of Technology Shenzhen
Original Assignee
Harbin Institute of Technology Shenzhen
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 Harbin Institute of Technology Shenzhen filed Critical Harbin Institute of Technology Shenzhen
Priority to CNB2005100097544A priority Critical patent/CN100355149C/en
Publication of CN1652400A publication Critical patent/CN1652400A/en
Application granted granted Critical
Publication of CN100355149C publication Critical patent/CN100355149C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Aerials With Secondary Devices (AREA)

Abstract

本发明公开一种移动通信用自适应天线。电压控制自适应天线由N个天线阵元和一个电波波束反射器10组成,10设置在天线阵元的侧面,天线阵元由引向器1、可变介质层体2、第一天线振子3、第二天线振子4、上电极5、下电极6和可调压直流电源7组成,3和4固定在2的朝向10的侧表面上,1固定在2的背向10的侧表面上,5固定在2的顶部,6固定在2的底部,7的两个输出端分别连接5和6,2中5和6连线方向的压电常数大于垂直其连线方向的压电常数。7向2施加电场,改变2的介电常数,从而使得电波通过介质的相位特性发生变化,最终改变了合成波束的方向。延时的控制不再需要数据存储,控制上非常容易实现。

Figure 200510009754

The invention discloses an adaptive antenna for mobile communication. The voltage control adaptive antenna is composed of N antenna array elements and a radio wave beam reflector 10, 10 is arranged on the side of the antenna array element, and the antenna array element is composed of a director 1, a variable dielectric layer 2, and a first antenna oscillator 3 , a second antenna vibrator 4, an upper electrode 5, a lower electrode 6 and an adjustable DC power supply 7, 3 and 4 are fixed on the side surface of 2 facing 10, 1 is fixed on the side surface of 2 facing away from 10, 5 is fixed on the top of 2, 6 is fixed on the bottom of 2, and the two output terminals of 7 are respectively connected to 5 and 6, and the piezoelectric constant in the direction of 5 and 6 in 2 is greater than that perpendicular to the direction of their connection. 7. Apply an electric field to 2 to change the dielectric constant of 2, so that the phase characteristics of the electric wave passing through the medium change, and finally change the direction of the synthesized beam. Delay control no longer requires data storage, and the control is very easy to implement.

Figure 200510009754

Description

电压控制自适应天线Voltage Controlled Adaptive Antenna

技术领域:Technical field:

本发明涉及一种移动通信用自适应天线。The invention relates to an adaptive antenna for mobile communication.

背景技术:Background technique:

一般的定向天线不能根据需要自动变换方向,为了能够适应用户移动等因素的要求,普通定向天线通过调整介质层厚度和天线振子距离金属反射板之间的距离来改变天线的波瓣,非常麻烦。电调谐定向天线采用信号相位(延时)调整,来加强特定方向的信号或抑制特定方向的信号,其基本结构如图1所示。目前的智能天线则采用多个相同阵元,通过调整不同阵元天线信号的相位(延时)来控制信号的合成相位,如图2所示,通过改变不同线阵元中延时调整电路中的具体延时数值,得到不同相位的电波波束,从而使得不同空间位置的信号互相加强或者抵消。具体过程是将输入的天线信号进行高速采样和计算以确定具体延时数值,这样做的难度是采样速度要求高,特别是针对通用的软件无线电平台,要求A/D和D/A越来越靠近高频(天线)端,延时地调整等效位数据的存储,存储量越大,可调延时的范围也越大,实现难度也随之增加,这个因素给软件无线电的实现带来困难。因此现有的智能天线的缺点是,在技术实现上需要采用高速的信号采样和计算,相位(延时)控制量容易受到影响,控制过程比较复杂。Ordinary directional antennas cannot automatically change direction according to needs. In order to adapt to the requirements of factors such as user movement, ordinary directional antennas change the lobes of the antenna by adjusting the thickness of the dielectric layer and the distance between the antenna oscillator and the metal reflector, which is very troublesome. The electrically tuned directional antenna uses signal phase (delay) adjustment to strengthen or suppress signals in a specific direction. Its basic structure is shown in Figure 1. The current smart antenna uses multiple same array elements, and controls the composite phase of the signal by adjusting the phase (delay) of antenna signals of different array elements, as shown in Figure 2, by changing the delay in different line array elements The specific delay value can be used to obtain radio wave beams with different phases, so that the signals at different spatial positions can strengthen or cancel each other. The specific process is to sample and calculate the input antenna signal at high speed to determine the specific delay value. The difficulty of this is that the sampling speed is high, especially for the general software radio platform, which requires A/D and D/A to be more and more Close to the high-frequency (antenna) end, adjust the storage of equivalent bit data with a delay. The larger the storage capacity, the larger the range of adjustable delay, and the difficulty of implementation increases. This factor brings the realization of software radio. difficulty. Therefore, the disadvantages of existing smart antennas are that high-speed signal sampling and calculation are required for technical implementation, the phase (delay) control amount is easily affected, and the control process is relatively complicated.

发明内容:Invention content:

本发明的目的是提供一种控制过程比较简单的电压控制自适应天线,以克服现有的智能天线在技术实现上需要采用高速的信号采样和计算,相位控制量容易受到影响,控制过程比较复杂的缺陷。本发明的技术方案是:它由N个天线阵元(A1~AN)和一个电波波束反射器10组成,电波波束反射器10设置在所有的天线阵元的侧面,每个天线阵元由引向器1、可变介质层体2、第一天线振子3、第二天线振子4、上电极5、下电极6和可调压直流电源7组成,第一天线振子3固定在可变介质层体2的朝向电波波束反射器10的侧表面的上部,第二天线振子4固定在可变介质层体2的朝向电波波束反射器10的侧表面的下部,引向器1固定在可变介质层体2的背向电波波束反射器10的侧表面上,上电极5固定在可变介质层体2的顶部,下电极6固定在可变介质层体2的底部,可调压直流电源7的两个输出端分别连接上电极5和下电极6,可变介质层体2中上电极5和下电极6连线方向的压电常数大于垂直于上电极5和下电极6连线方向的压电常数。本发明的天线工作时,在第一天线振子3和第二天线振子4之间输入发射信号并产生电磁波,在电波波束反射器10的反射作用下向外发射无线电波,由于每个天线阵元中都单独设置了可调压直流电源7,可调压直流电源7通过上电极5和下电极6向可变介质层体2施加电场,改变可变介质层体2的介电常数,从而使得电波通过介质的相位特性发生变化,通过这样的方式等效为延时调整,最终改变了合成波束的方向。当采用电压控制之后,延时的控制不再需要数据存储,而是通过介电常数的变化,改变电波的传播速度,技术上同样起到延时作用,但控制上非常容易实现,不再需要存储大量数据。因此,控制较传统方式简化。本发明结构简单、设计合理、工作可靠,具有较大的推广价值。The purpose of the present invention is to provide a voltage control adaptive antenna with a relatively simple control process to overcome the need for high-speed signal sampling and calculation in the technical implementation of existing smart antennas, the phase control amount is easily affected, and the control process is relatively complicated Defects. The technical scheme of the present invention is: it is made up of N antenna array elements (A1~AN) and a radio wave beam reflector 10, and radio wave beam reflector 10 is arranged on the side of all antenna array elements, and each antenna array element is led by Composed of a directing device 1, a variable dielectric layer 2, a first antenna element 3, a second antenna element 4, an upper electrode 5, a lower electrode 6, and an adjustable voltage DC power supply 7, the first antenna element 3 is fixed on the variable dielectric layer The upper part of the side surface of the body 2 towards the radio wave beam reflector 10, the second antenna vibrator 4 is fixed on the lower part of the side surface of the variable medium layer body 2 towards the radio wave beam reflector 10, and the director 1 is fixed on the variable medium On the side surface of the layer body 2 facing away from the radio wave beam reflector 10, the upper electrode 5 is fixed on the top of the variable medium layer body 2, the lower electrode 6 is fixed on the bottom of the variable medium layer body 2, and the adjustable voltage DC power supply 7 The two output ends of the two output terminals are respectively connected to the upper electrode 5 and the lower electrode 6, and the piezoelectric constant in the direction of the upper electrode 5 and the lower electrode 6 in the variable medium layer body 2 is greater than that perpendicular to the direction of the upper electrode 5 and the lower electrode 6. piezoelectric constant. When the antenna of the present invention works, a transmission signal is input between the first antenna element 3 and the second antenna element 4 and electromagnetic waves are generated, and radio waves are emitted outwards under the reflection of the radio wave beam reflector 10, because each antenna array element The adjustable voltage direct current power supply 7 is set separately in each of them, and the adjustable voltage direct current power supply 7 applies an electric field to the variable medium layer body 2 through the upper electrode 5 and the lower electrode 6 to change the dielectric constant of the variable medium layer body 2, so that The phase characteristics of the radio wave passing through the medium change, which is equivalent to a delay adjustment, and finally changes the direction of the synthesized beam. When the voltage control is adopted, the delay control no longer needs data storage, but changes the propagation speed of the electric wave through the change of the dielectric constant, which also plays a role in delay technically, but the control is very easy to implement and no longer needs Store large amounts of data. Therefore, the control is simplified compared with the traditional way. The invention has the advantages of simple structure, reasonable design, reliable operation and great popularization value.

附图说明:Description of drawings:

图1和图2是已有的天线结构示意图,图3是本发明的结构示意图,图4是图3的俯视图。FIG. 1 and FIG. 2 are schematic structural diagrams of existing antennas, FIG. 3 is a schematic structural diagram of the present invention, and FIG. 4 is a top view of FIG. 3 .

具体实施方式:Detailed ways:

下面结合图3和图4具体说明本实施方式。本实施方式由N个天线阵元(A1~AN)和一个电波波束反射器10组成,N个天线阵元(A1~AN)排列成一行,电波波束反射器10设置在所有的天线阵元的侧面,每个天线阵元由引向器1、可变介质层体2、第一天线振子3、第二天线振子4、上电极5、下电极6和可调压直流电源7组成,第一天线振子3固定在可变介质层体2的朝向电波波束反射器10的侧表面的上部,第二天线振子4固定在可变介质层体2的朝向电波波束反射器10的侧表面的下部,引向器1固定在可变介质层体2的背向电波波束反射器10的侧表面上,上电极5固定在可变介质层体2的顶部,下电极6固定在可变介质层体2的底部,可调压直流电源7的两个输出端分别连接上电极5和下电极6,可变介质层体2中上电极5和下电极6连线方向的压电常数大于垂直于上电极5和下电极6连线方向的压电常数。可变介质层体2的材料选用介电常数可变的非线性材料,例如液晶或等离子材料。由于对电波波束的控制方位需要有大的变化范围,希望可变介质层体2选用介电常数变化范围大的材料,液晶和等离子材料等的介电常数随着外加电压的变化而变化,在控制电压的作用下变化范围较大。上电极5与下电极6之间距离越远,需要可调压直流电源7输出的控制电压也越高。目前的小范围覆盖的微型天线,可以使用较低的控制电压,就能满足波束的扫描使用。例如,在民用通信中,工作在2G~3GHz频段的天线,在单一振源方向性部做特定要求条件下,上电极5与下电极6之间的距离为10cm,同时可变介质层体2使用的是液晶材料,可调压直流电源7变化范围大约几十伏到900伏之间即可,此时介电常数的变化范围可以从几百到几千(例如500到2000)。考虑电磁波的传播速度与介电常数的关系,做一个粗略估计,如果介电常数变化4倍,例如在上电极5与下电极6之间的距离10cm,可变介质层体2的厚度为1cm的介质层中,相位的差别大约π/2。这样的波束扫描大约可以达到2π/3,从而得到不同的方向性。以上假设估算,没有考虑频段、天线尺寸、单一振源方向性等指标的变化,针对具体天线,需要具体计算。This embodiment will be described in detail below with reference to FIG. 3 and FIG. 4 . This embodiment is composed of N antenna array elements (A1~AN) and a radio wave beam reflector 10, the N antenna array elements (A1~AN) are arranged in a row, and the radio wave beam reflector 10 is arranged on all antenna array elements On the side, each antenna element is composed of a director 1, a variable dielectric layer 2, a first antenna element 3, a second antenna element 4, an upper electrode 5, a lower electrode 6, and an adjustable DC power supply 7. The first Antenna vibrator 3 is fixed on the upper part of the variable medium layer body 2 towards the side surface of the radio wave beam reflector 10, and the second antenna vibrator 4 is fixed on the lower part of the variable medium layer body 2 towards the side surface of the radio wave beam reflector 10, The director 1 is fixed on the side surface of the variable medium layer 2 facing away from the radio wave beam reflector 10, the upper electrode 5 is fixed on the top of the variable medium layer 2, and the lower electrode 6 is fixed on the variable medium layer 2 The bottom of the adjustable voltage DC power supply 7 is connected to the upper electrode 5 and the lower electrode 6 respectively, and the piezoelectric constant in the direction of the upper electrode 5 and the lower electrode 6 in the variable medium layer 2 is greater than that perpendicular to the upper electrode 5 and the piezoelectric constant of the connection direction of the lower electrode 6. The material of the variable medium layer 2 is a non-linear material with variable dielectric constant, such as liquid crystal or plasma material. Since the control orientation of the radio wave beam needs to have a large range of variation, it is hoped that the variable dielectric layer body 2 will select a material with a large range of dielectric constant variation, and the dielectric constant of liquid crystal and plasma materials will change with the change of the applied voltage. Under the action of the control voltage, the range of change is relatively large. The farther the distance between the upper electrode 5 and the lower electrode 6 is, the higher the control voltage output by the adjustable voltage DC power supply 7 is. The current micro-antenna covering a small area can use a lower control voltage to meet the scanning requirements of the beam. For example, in civil communication, for antennas working in the 2G-3GHz frequency band, under the condition that the directivity of a single vibration source is specified, the distance between the upper electrode 5 and the lower electrode 6 is 10cm, and the variable dielectric layer 2 Liquid crystal material is used, and the variable range of the adjustable voltage DC power supply 7 is about tens of volts to 900 volts. At this time, the range of dielectric constant can be from hundreds to thousands (for example, 500 to 2000). Consider the relationship between the propagation speed of electromagnetic waves and the dielectric constant, and make a rough estimate. If the dielectric constant changes by 4 times, for example, the distance between the upper electrode 5 and the lower electrode 6 is 10 cm, and the thickness of the variable dielectric layer 2 is 1 cm. In the dielectric layer, the phase difference is about π/2. Such beam scanning can reach approximately 2π/3, resulting in different directivities. The above hypothetical estimation does not take into account the changes in the frequency band, antenna size, and directivity of a single vibration source. For specific antennas, specific calculations are required.

本发明将不同的定向天线进行修改,在天线振子和引相器之间的介质层上下端增加2个正负电极,通过对电极上直流电压的改变,改变压电介质的介电常数,从而使得电波通过介质的相位特性发生变化,最终改变了合成波束的方向,通过这样的方式虽然等效为延时调整,但是控制过程和参数简化。接受波束的方向控制与发射波束的方向控制相同。考虑到对电场的敏感性需求,可变介质层体2材料上使用非各相同性的介质,使可变介质层体2的介电常数敏感于上电极5与下电极6之间外加电压的变化,而不敏感与垂直二者的方向。与传统的天线相比,采用了传统的信号估计方法,但是不需要对每个信号单独调整延时,简化了计算量。天线中的阵元数量n可变,通过调整n数值来改变天线的波瓣宽度,n越大,波瓣越窄,方向性越好。电压的变化直接控制合成波瓣的角度。In the present invention, different directional antennas are modified, and two positive and negative electrodes are added to the upper and lower ends of the dielectric layer between the antenna vibrator and the phase guider, and the dielectric constant of the piezoelectric medium is changed by changing the DC voltage on the electrodes, thereby The phase characteristics of the radio wave passing through the medium are changed, and finally the direction of the synthesized beam is changed. Although this method is equivalent to delay adjustment, the control process and parameters are simplified. Steering of the receive beam is the same as that of the transmit beam. In consideration of the sensitivity requirement to the electric field, a non-isotropic medium is used on the material of the variable dielectric layer 2, so that the dielectric constant of the variable dielectric layer 2 is sensitive to the applied voltage between the upper electrode 5 and the lower electrode 6. Variations are insensitive to both orientation and vertical. Compared with the traditional antenna, the traditional signal estimation method is adopted, but there is no need to adjust the delay for each signal separately, which simplifies the calculation amount. The number n of array elements in the antenna is variable, and the lobe width of the antenna can be changed by adjusting the value of n. The larger n is, the narrower the lobes are and the better the directivity is. The change in voltage directly controls the angle of the composite lobe.

Claims (2)

1, voltage control adaptive aerial, it is by N bay (A1~AN) form with an electric wave beam reflector (10), electric wave beam reflector (10) is arranged on the side of all bays, it is characterized in that each bay is by director (1), variable dielectric layer body (2), first antenna oscillator (3), second antenna oscillator (4), top electrode (5), bottom electrode (6) and tunable voltage dc power supply (7) are formed, first antenna oscillator (3) is fixed on the top towards the side surface of electric wave beam reflector (10) of variable dielectric layer body (2), second antenna oscillator (4) is fixed on the bottom towards the side surface of electric wave beam reflector (10) of variable dielectric layer body (2), director (1) is fixed on the side surface of the beam reflector of electric wave dorsad (10) of variable dielectric layer body (2), top electrode (5) is fixed on the top of variable dielectric layer body (2), bottom electrode (6) is fixed on the bottom of variable dielectric layer body (2), the piezoelectric constant of top electrode (5) and bottom electrode (6) line direction is greater than the piezoelectric constant perpendicular to top electrode (5) and bottom electrode (6) line direction in two outputs of tunable voltage dc power supply (7) Connect Power the respectively utmost point (5) and the bottom electrode (6), variable dielectric layer body (2).
2, voltage control adaptive aerial according to claim 1 is characterized in that the material selection liquid crystal or the plasma material of variable dielectric layer body (2).
CNB2005100097544A 2005-02-18 2005-02-18 Voltage control adaptive aerial Expired - Fee Related CN100355149C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNB2005100097544A CN100355149C (en) 2005-02-18 2005-02-18 Voltage control adaptive aerial

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB2005100097544A CN100355149C (en) 2005-02-18 2005-02-18 Voltage control adaptive aerial

Publications (2)

Publication Number Publication Date
CN1652400A true CN1652400A (en) 2005-08-10
CN100355149C CN100355149C (en) 2007-12-12

Family

ID=34875438

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2005100097544A Expired - Fee Related CN100355149C (en) 2005-02-18 2005-02-18 Voltage control adaptive aerial

Country Status (1)

Country Link
CN (1) CN100355149C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1881685B (en) * 2006-03-22 2010-05-12 北京航空航天大学 Cross-feed Broadband Printed Yagi Antenna
CN102971910A (en) * 2012-01-21 2013-03-13 华为技术有限公司 Antenna Units and Antennas

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1150380B1 (en) * 1998-12-14 2006-05-31 Matsushita Electric Industrial Co., Ltd. Active phased array antenna and antenna controller
US20030184477A1 (en) * 2002-03-29 2003-10-02 Lotfollah Shafai Phased array antenna steering arrangements
US6856216B1 (en) * 2003-10-06 2005-02-15 Harris Corporation Sample-and-hold phase shifter control voltage distribution in a phased array utilizing voltage-controlled phase shift devices

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1881685B (en) * 2006-03-22 2010-05-12 北京航空航天大学 Cross-feed Broadband Printed Yagi Antenna
CN102971910A (en) * 2012-01-21 2013-03-13 华为技术有限公司 Antenna Units and Antennas
CN102971910B (en) * 2012-01-21 2015-12-23 华为技术有限公司 Antenna Units and Antennas

Also Published As

Publication number Publication date
CN100355149C (en) 2007-12-12

Similar Documents

Publication Publication Date Title
JP6786627B2 (en) Antenna integrated with photovoltaic cell
US10727823B2 (en) Method for adjusting electromagnetic wave, and metamaterial
KR102576115B1 (en) Electronic devices with probe-fed dielectric resonator antennas
EP3928380B1 (en) Switchable patch antenna
JP6980768B2 (en) Impedance matching for open surface antennas
KR20160008457A (en) Metamaterial-based phase shifting element and phased array
JP2019502311A (en) Distributed direct drive for driving cells
JP2018507653A (en) Antenna element arrangement of cylindrical feed antenna
JP6974429B2 (en) Internal heater for RF opening
JP2019517222A (en) Thin communication terminal and method of providing thin communication terminal
KR102374153B1 (en) Liquid crystal-based reflective metasurface, and reflective array antenna and antenna device comprising the same
KR20230157321A (en) Metasurface antenna with integrated varactor circuit
KR20220031625A (en) ground plane heater
TWI885094B (en) Electrical addressing for a metamaterial radio-frequency (rf) antenna
CN108767485B (en) A Planar Microstrip Transmission Array Antenna
EP3422477B1 (en) Liquid-crystal antenna apparatus and method for tracking wireless apparatus using the same
CN100355149C (en) Voltage control adaptive aerial
US12040550B2 (en) Cell rotation and frequency compensation in diode designs
JP2022526029A (en) Non-circular center feed antenna and method using this antenna
KR101751123B1 (en) Reflect Type Cell Array Antenna with Small Size
CN209119366U (en) A phased array antenna
KR20210044729A (en) Liquid crystal based frequency reconfigurable prs antenna system
CN206673120U (en) A kind of deposited copper PCB Double-frequency antenna structure
Rzymowski et al. Design, realization and measurements of enhanced performance 2.4 GHz ESPAR antenna for localization in wireless sensor networks
US20250038400A1 (en) Beam-steering antenna systems

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
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20071212

Termination date: 20110218