CN106450709B - Four-unit interconnected symmetrical oscillator circular antenna array for electric small-distance direction finding - Google Patents
Four-unit interconnected symmetrical oscillator circular antenna array for electric small-distance direction finding Download PDFInfo
- Publication number
- CN106450709B CN106450709B CN201611200989.6A CN201611200989A CN106450709B CN 106450709 B CN106450709 B CN 106450709B CN 201611200989 A CN201611200989 A CN 201611200989A CN 106450709 B CN106450709 B CN 106450709B
- Authority
- CN
- China
- Prior art keywords
- antenna
- symmetrical
- connection section
- section structure
- array
- 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
Links
- 239000000463 material Substances 0.000 claims abstract description 4
- 239000007769 metal material Substances 0.000 claims abstract description 4
- 230000008878 coupling Effects 0.000 claims description 19
- 238000010168 coupling process Methods 0.000 claims description 19
- 238000005859 coupling reaction Methods 0.000 claims description 19
- 239000002184 metal Substances 0.000 claims description 2
- 230000005855 radiation Effects 0.000 abstract description 6
- 238000005516 engineering process Methods 0.000 description 8
- 230000008859 change Effects 0.000 description 7
- 238000010586 diagram Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 238000005259 measurement Methods 0.000 description 4
- 230000035945 sensitivity Effects 0.000 description 4
- 238000004422 calculation algorithm Methods 0.000 description 3
- 238000001228 spectrum Methods 0.000 description 3
- 238000003491 array Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000004088 simulation Methods 0.000 description 2
- 238000000342 Monte Carlo simulation Methods 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 238000007635 classification algorithm Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000005284 excitation Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/36—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/50—Structural association of antennas with earthing switches, lead-in devices or lightning protectors
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
Landscapes
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
用于电小间距测向的四单元互连对称振子圆环天线阵列,涉及阵列天线。包括4个对称振子结构天线和2个天线连接段结构;所述4个对称振子结构天线以圆环阵的方式均匀排布,其中4个对称振子的上、下两部分结构各自使用天线连接段结构直接相连,电小间距是指相邻单元的间距远小于工作波长,辐射单元包括4个材料和尺寸相同的对称振子结构在同一参考面平行摆放,且以圆环阵的方式均匀等角度间隔排布;所述天线连接段结构是4个对称振子结构的上半部分使用天线连接段结构直接相连,下半部分使用同样的天线连接段结构直接相连,天线连接段结构是四段圆柱体结构按照正四边形连接形成的连接结构;天线连接段结构与对称振子使用等直径相同金属材料。
The invention relates to a four-element interconnected symmetrical dipole circular loop antenna array for direction finding with an electrically small spacing, relating to an array antenna. It includes 4 symmetrical dipole structure antennas and 2 antenna connection section structures; the 4 symmetrical dipole structure antennas are evenly arranged in a circular array, and the upper and lower parts of the 4 symmetrical dipole structures use antenna connection sections respectively The structure is directly connected, and the electric small spacing means that the spacing between adjacent units is much smaller than the working wavelength. The radiation unit includes 4 symmetrical oscillator structures with the same material and size, which are placed in parallel on the same reference plane, and are evenly angled in a circular array. Arranged at intervals; the antenna connection section structure is 4 symmetrical oscillator structures, the upper part is directly connected with the antenna connection section structure, and the lower part is directly connected with the same antenna connection section structure, and the antenna connection section structure is four cylinders The structure is a connection structure formed by regular quadrilateral connection; the antenna connection section structure and the symmetrical vibrator use the same metal material with the same diameter.
Description
技术领域technical field
本发明涉及阵列天线,尤其是涉及一种用于超分辨来波达到角(Direction ofArrival,DOA)估计的电小间距阵列天线设计。The present invention relates to array antennas, in particular to an electrically small-pitch array antenna design for super-resolution estimation of arrival angle (Direction of Arrival, DOA).
背景技术Background technique
空间谱估计用来解决接收信号的空间能量分布问题,以此来确定信号的数目或者信号的来波方向([1]王永良,丁前军,李荣锋.自适应整理处理[M].北京:清华大学出版社,2009;[2]王永良,陈辉,彭应宁,万群.空间谱估计理论与算法[M].北京:清华大学出版社,2004)来波方向估计也称为到达角估计([3]Haykin S,Liu K J R.Handbook on arrayprocessing and sensor networks[M].John Wiley&Sons,2010)。来波方向估计所关心的问题是找到空间中辐射源的位置。一般来说,来波方向估计主要包括两方面的内容:(1)确定空间中辐射源的个数;(2)确定每个辐射源的空间位置。随着测向技术的发展,针对不同的问题,已经发展出很多的方法。测向技术从主被动侦察(或者天线类型)的角度可以分为有源测向技术和无源测向技术。通过发射电磁波,并且通过接收目标散射信号来获取目标的距离和方位的测向方法称为有源测向技术。由于有源测向技术的系统有主动辐射设备,这样就暴露了有源测向系统的空间位置,很容易被其他设备进行侦察并定位,这对于军事应用而言是致命的。无源测向技术由于具有高度的保密性而越来越受到人们的青睐,并得到了广泛的发展。利用两单元或多单元阵列天线来测定电磁波的来波到达角即无源测向技术,具有多方面的重要用途([4]Stephen E.Lipsky.Microwave passive directionfinding[M].Scitech Pub Inc.,2003)。Spatial spectrum estimation is used to solve the problem of spatial energy distribution of received signals, so as to determine the number of signals or the direction of arrival of signals ([1] Wang Yongliang, Ding Qianjun, Li Rongfeng. Adaptive processing [M]. Beijing: Tsinghua University University Press, 2009; [2] Wang Yongliang, Chen Hui, Peng Yingning, Wan Qun. Spatial Spectrum Estimation Theory and Algorithm [M]. Beijing: Tsinghua University Press, 2004) The direction of arrival estimation is also called the angle of arrival estimation ([ 3] Haykin S, Liu K J R. Handbook on array processing and sensor networks [M]. John Wiley & Sons, 2010). Direction of arrival estimation is concerned with finding the position of a radiation source in space. Generally speaking, direction of arrival estimation mainly includes two aspects: (1) determining the number of radiation sources in space; (2) determining the spatial position of each radiation source. With the development of direction finding technology, many methods have been developed for different problems. Direction finding technology can be divided into active direction finding technology and passive direction finding technology from the perspective of active and passive reconnaissance (or antenna type). The direction-finding method that obtains the distance and azimuth of the target by emitting electromagnetic waves and receiving the scattered signals of the target is called active direction-finding technology. Since the active direction finding technology system has active radiation equipment, the spatial position of the active direction finding system is exposed, and it is easy to be detected and positioned by other equipment, which is fatal for military applications. Passive direction finding technology is more and more favored by people because of its high degree of confidentiality, and has been widely developed. Using two-unit or multi-unit array antennas to measure the arrival angle of electromagnetic waves, that is, passive direction finding technology, has many important uses ([4]Stephen E.Lipsky.Microwave passive directionfinding[M].Scitech Pub Inc., 2003).
电小间距阵列是指阵列间距远远小于波长(一般为0.1倍波长或者更小)的阵列系统。这种阵列可以将传统的阵列缩小到1/10,能够极大的降低阵列的尺寸。但是,小型化与测向精度之间会产生一对矛盾。阵列尺寸变小,会使阵列的增益变低,信噪比下降。单元间距变小,单元之间的相位差变化就比较缓慢。加上阵元之间的强烈的电磁耦合([5]HansenR C.Electrically small,superdirective,and superconducting antennas[M].JohnWiley&Sons,2006),影响了阵列天线的实际性能,使得传统的电小间距阵列在仅依靠改进算法的情况下仍然无法满足高精度的测向要求。低增益和小相位差是限制电小天线测向发展与应用的技术瓶颈。因此,发展基于新机理的高精度电小间距阵列具有重大的现实意义。Electrically fine-pitch arrays refer to array systems in which the array pitch is much smaller than the wavelength (generally 0.1 times the wavelength or less). This array can shrink the traditional array to 1/10, which can greatly reduce the size of the array. However, there will be a pair of contradictions between miniaturization and direction finding accuracy. The smaller the size of the array, the lower the gain of the array and the lower the signal-to-noise ratio. The smaller the cell pitch, the slower the phase difference between the cells changes. Coupled with the strong electromagnetic coupling between array elements ([5]HansenR C. Electrically small, superdirective, and superconducting antennas[M].JohnWiley&Sons, 2006), it affects the actual performance of the array antenna, making the traditional electrically small spacing array in Only relying on the improved algorithm still cannot meet the high-precision direction finding requirements. Low gain and small phase difference are the technical bottlenecks that limit the development and application of direction finding for electrically small antennas. Therefore, it is of great practical significance to develop high-precision electrically fine-pitch arrays based on new mechanisms.
中国专利201610350399.5本发明公开一种双环天线,利用振幅法测向,并通过相互垂直的两个方向的第一天线环体和第二天线环体同时接收信号以进行计算而精确判断电磁波发射源的方向,从而有效提高入射波方向角的分辨率,进而有效提高测量精确度;且由于为垂直并同轴心嵌套连接的双环结构,因此体积也相对较小([6]陆德坚,袁迪.双环天线[P].北京:CN105870631A,2016-08-17)。Chinese patent 201610350399.5 The present invention discloses a double-loop antenna, which uses the amplitude method to measure direction, and simultaneously receives signals through the first antenna loop body and the second antenna loop body in two directions perpendicular to each other for calculation to accurately determine the source of electromagnetic wave emission direction, so as to effectively improve the resolution of the incident wave direction angle, thereby effectively improving the measurement accuracy; and because it is a double-ring structure that is vertical and nested with the coaxial center, the volume is relatively small ([6] Lu Dejian, Yuan Di. Double loop antenna [P]. Beijing: CN105870631A, 2016-08-17).
中国专利201410080935.5公开了一种相位干涉仪的无源测向天线阵及相位干涉仪([7]艾礼科,莫绍辉,甄银彪,姚士刚,赵亲成,王志彬,张海涛.相位干涉仪的无源测向天线阵及相位干涉仪[P].广东:CN103887613A,2014-06-25),其发明第一层圆形天线阵可以包含有多个双极化全向天线阵元,因此在测向过程中,相位差的组合也就更多,更加有利于提高测向的精度,减少复杂环境的影响。Chinese patent 201410080935.5 discloses a passive direction-finding antenna array of a phase interferometer and a phase interferometer ([7] Ai Like, Mo Shaohui, Zhen Yinbiao, Yao Shigang, Zhao Qincheng, Wang Zhibin, Zhang Haitao. Passive measurement of a phase interferometer Directional antenna array and phase interferometer [P]. Guangdong: CN103887613A, 2014-06-25), the first circular antenna array invented by it can contain multiple dual-polarized omnidirectional antenna elements, so in the direction finding process Among them, there are more combinations of phase differences, which is more conducive to improving the accuracy of direction finding and reducing the influence of complex environments.
中国专利201410347386.3公开了一种新型便携式五天线元测向圆阵([8]郭方,谭德鑫.新型便携式五天线元测向圆阵[P].四川:CN104167613A,2014-11-26),其目的在于提供一种体积小,重量轻,能快速拆装并可以同时满足干涉仪、相关干涉仪、空间谱估计等多种测向体制要求的五天线元测向圆阵。Chinese patent 201410347386.3 discloses a new portable five-antenna element direction-finding circular array ([8] Guo Fang, Tan Dexin. New portable five-antenna element direction-finding circular array [P]. Sichuan: CN104167613A, 2014-11-26), which The purpose is to provide a five-antenna-element direction-finding circular array that is small in size, light in weight, can be quickly disassembled, and can simultaneously meet the requirements of various direction-finding systems such as interferometers, correlation interferometers, and spatial spectrum estimation.
上述三篇专利均涉及的测向天线结构,虽然考虑了小型化、简单结构等因素,但不适用于在空间受限平台或低频段的情况。The direction-finding antenna structures involved in the above three patents are not suitable for space-constrained platforms or low-frequency bands, although factors such as miniaturization and simple structure have been considered.
发明内容Contents of the invention
本发明的目的在于针对电小间距阵列存在的上述问题,提供将整个电小间距对称振子阵列连成一个整体,可以增强电小间距对称振子阵列天线之间的电磁耦合,提高天线响应对于来波到达角的敏感度,从而提高来波到达角的测量精度,并可以适用于空间受限平台或低频信号的来波方向测量,对于测向设备小型化、结构简单化、便携易操作具有重要意义的用于电小间距测向的四单元互连对称振子圆环天线阵列。The purpose of the present invention is to solve the above-mentioned problems existing in the electrically small-pitch array, and provide a whole that connects the entire electrically small-pitch symmetric dipole array into a whole, which can enhance the electromagnetic coupling between the electrically small-pitch symmetric dipole array antennas, and improve the response of the antenna to incoming waves. The sensitivity of the angle of arrival, thereby improving the measurement accuracy of the angle of arrival of incoming waves, and can be applied to the measurement of the direction of arrival of space-constrained platforms or low-frequency signals, which is of great significance for the miniaturization, simple structure, portable and easy operation of direction-finding equipment A four-element interconnected symmetrical dipole circular loop antenna array for electrically small spacing direction finding.
本发明包括4个对称振子结构天线和2个天线连接段结构;The present invention includes four symmetrical oscillator structure antennas and two antenna connection section structures;
所述4个对称振子结构天线以圆环阵的方式均匀排布,其中4个对称振子的上、下两部分结构各自使用天线连接段结构直接相连,电小间距是指相邻单元的间距远小于工作波长,辐射单元包括4个材料和尺寸相同的对称振子结构在同一参考面平行摆放,且以圆环阵的方式均匀等角度间隔排布;所述天线连接段结构是4个对称振子结构的上半部分使用天线连接段结构直接相连,下半部分使用同样的天线连接段结构直接相连,天线连接段结构是四段圆柱体结构按照正四边形连接形成的连接结构;天线连接段结构与对称振子使用等直径相同金属材料。The four symmetrical oscillator structure antennas are evenly arranged in a circular array, wherein the upper and lower structures of the four symmetrical oscillators are directly connected by the antenna connection section structure, and the electrically small spacing means that the distance between adjacent units is far Smaller than the working wavelength, the radiating unit includes 4 symmetrical oscillator structures of the same material and size, which are placed in parallel on the same reference plane, and are arranged at equal angular intervals in a circular array; the antenna connection section structure is 4 symmetrical oscillators The upper part of the structure is directly connected with the antenna connection section structure, and the lower part is directly connected with the same antenna connection section structure. The antenna connection section structure is a connection structure formed by connecting four cylinder structures according to a regular quadrilateral; the antenna connection section structure and The symmetrical vibrator uses the same metal material with the same diameter.
天线连接段结构分别位于4个对称振子的上、下两部分的最靠近对称振子中部的金属末端,且天线连接段结构与对称振子主体垂直,形成上下两个整体部分,构成新的天线结构单元,以加强对称振子之间的电磁耦合。The antenna connecting section structure is respectively located at the metal ends of the upper and lower parts of the four symmetrical oscillators, which are closest to the middle of the symmetrical oscillator, and the antenna connecting section structure is perpendicular to the main body of the symmetrical oscillator, forming two integral parts up and down, forming a new antenna structure unit , to strengthen the electromagnetic coupling between the symmetric oscillators.
本发明的激励位置与传统对称振子激励位置相同,均在振子天线上下两臂之间。且四单元对称振子圆环阵单个单元的幅度和相位方向图随对称振子上、下两部分天线连接段结构间隔距离变化大,随着对称振子上、下两部分天线连接段结构间隔距离的增大,幅度和相位的变化随观测角的变化越来越缓慢,需要应用基于有源单元的全波电磁仿真来扫描参数搜寻最优对称振子上、下两部分天线连接段结构间隔距离,使得天线单元之间的电磁耦合最强,能量主要被电磁耦合到其他的单元方向上。The excitation position of the present invention is the same as that of the traditional symmetrical vibrator, which are both between the upper and lower arms of the vibrator antenna. Moreover, the amplitude and phase pattern of a single unit of the four-element symmetrical dipole ring array vary greatly with the distance between the upper and lower antenna connection sections of the symmetrical dipole. Large, the change of amplitude and phase becomes slower and slower with the change of observation angle. It is necessary to apply the full-wave electromagnetic simulation based on the active unit to scan the parameters to search for the optimal distance between the upper and lower antenna connection sections of the symmetrical oscillator, so that the antenna The electromagnetic coupling between the elements is the strongest, and the energy is mainly electromagnetically coupled to other element directions.
直连对称振子阵列的增益相对于非直连情况有明显增强,天线单元的实际增益有明显的提高,且方向性更强,在不同的观测角下增益的变化更为剧烈,即提高单元增益和相位差对于目标信号来波到达角的敏感度。在整个方位角的变化范围内,电小间距四单元直连对称振子圆环阵列天线的对称性会导致来波到达角方向估计的克拉CRB远低于非直连情况,即测向精度有显著的提高。The gain of the directly connected symmetric dipole array is significantly enhanced compared with the non-directly connected situation, the actual gain of the antenna unit is significantly improved, and the directionality is stronger, and the change of the gain is more drastic under different observation angles, that is, to increase the unit gain and the sensitivity of the phase difference to the arrival angle of the target signal. In the entire range of azimuth angle variation, the symmetry of the electrically small-pitch four-element direct-connected symmetrical dipole circular ring array antenna will cause the CRB of the direction estimation of the incoming wave arrival angle to be much lower than that of the non-direct connection case, that is, the direction-finding accuracy has a significant improvement.
本发明的优点和积极效果在于:此种拓扑结构天线阵列,即单元之间的互连结构,会增加单元之间的电磁耦合,提高单元之间方向图幅度和相位差之间的变化,从而提高天线阵元对于目标信号来波方向的敏感度,从而提高测向精度。The advantages and positive effects of the present invention are: this topology antenna array, that is, the interconnection structure between the units, can increase the electromagnetic coupling between the units, improve the variation between the pattern amplitude and the phase difference between the units, and thus Improve the sensitivity of the antenna array element to the incoming wave direction of the target signal, thereby improving the direction finding accuracy.
附图说明Description of drawings
图1为本发明实施例的主视结构示意图。Fig. 1 is a schematic diagram of the structure of the front view of the embodiment of the present invention.
图2为本发明实施例的俯视结构示意图。Fig. 2 is a top view structural diagram of an embodiment of the present invention.
图3为实施例对于不同的对称振子上下间隔距离且在振子直径为0.1λ时的S11参数比较。Fig. 3 is a comparison of the S11 parameters of the embodiment for different vertical distances between the symmetrical vibrator and when the diameter of the vibrator is 0.1λ.
图4为本发明实施例对称振子上下间隔距离且在振子直径在0.1λ时的天线单元1的幅度比较。FIG. 4 is a comparison of the amplitudes of the antenna unit 1 when the vibrator diameter is 0.1λ with a symmetrical vibrator spaced apart from top to bottom according to an embodiment of the present invention.
图5为本发明实施例对称振子上下间隔距离且在振子直径在0.1λ时的天线单元1的相位方向图比较。FIG. 5 is a comparison of the phase pattern diagrams of the antenna unit 1 when the symmetrical dipoles are spaced vertically apart and the diameter of the dipole is 0.1λ according to the embodiment of the present invention.
图6为本发明实施例在振子直径为0.1λ时同考虑电磁耦合未直连的同参数天线阵的S参数比较。Fig. 6 is a comparison of the S parameters of an antenna array with the same parameters but not directly connected in consideration of electromagnetic coupling when the diameter of the vibrator is 0.1λ according to the embodiment of the present invention.
图7为本发明实施例在振子直径为0.1λ时的天线单元1的方向图。FIG. 7 is a directional diagram of the antenna unit 1 when the dipole diameter is 0.1λ according to the embodiment of the present invention.
图8为本发明实施例在振子直径为0.1λ时的相位差变化Fig. 8 shows the phase difference change when the vibrator diameter is 0.1λ according to the embodiment of the present invention
图9为本发明实施例在振子直径为0.1λ时在信噪比SNR=15dB,采样频率是三倍工作频率,即fs=3f0,且快拍数K=300与考虑电磁耦合未直连的同参数天线阵进行次蒙特卡洛模拟的DOA均方差对比图。Figure 9 shows the embodiment of the present invention when the vibrator diameter is 0.1λ, the signal-to-noise ratio SNR=15dB, the sampling frequency is three times the operating frequency, that is, f s =3f 0 , and the number of snapshots K=300 is not directly related to the consideration of electromagnetic coupling Comparison chart of mean square error of DOA for sub-Monte Carlo simulation of the same parameter antenna array.
图10为本发明实施例的立体结构示意图。Fig. 10 is a schematic perspective view of the three-dimensional structure of the embodiment of the present invention.
具体实施方式Detailed ways
本发明提供了一种基于振子互连的电小间距对称振子阵列天线结构,为了使本发明的目的、技术方案及优点更加清楚明白,以下结合附图及实施例,对本发明进行进一步详细说明。应当理解,此处所描述的具体实施例仅仅用以解释本发明,并不用于限定本发明。具体实现步骤如下:The present invention provides an electrically small-pitch symmetric dipole array antenna structure based on dipole interconnection. In order to make the purpose, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. The specific implementation steps are as follows:
1)以直径为0.1λ四单元电小间距对称振子阵列天线为例1) Take the symmetric dipole array antenna with a diameter of 0.1λ as an example
2)其参数设定为单元天线在xOy平面内,如图1所示,四个材料、尺寸相同的对称振子结构天线:天线单元1、天线单元2、天线单元3、天线单元4在以原点为圆心,工作频率是1GHz,对应直径为0.1倍波长,即ΦARRAY=0.1λ=30mm的圆环上排布,振子半径R=0.05λ=1.5mm;四个振子的长度由半波对称振子基础模型通过优化得到L=69mm;每个单元的端口采以用73.2Ω的阻抗加载,相当于负载。2) Its parameters are set so that the unit antenna is in the xOy plane, as shown in Figure 1, four symmetrical oscillator structure antennas with the same material and size: antenna unit 1, antenna unit 2, antenna unit 3, and antenna unit 4 are at the origin As the center of the circle, the operating frequency is 1GHz, and the corresponding diameter is 0.1 times the wavelength, that is, Φ ARRAY = 0.1λ = 30mm Arranged on a circle, the vibrator radius R = 0.05λ = 1.5mm; the length of the four vibrators is determined by the half-wave symmetrical vibrator The basic model is optimized to obtain L = 69mm; the port of each unit is loaded with an impedance of 73.2Ω, which is equivalent to the load.
3)天线连接段结构是四个对称振子结构的上半部分使用天线连接段结构直接相连,下半部分使用同样的天线连接段结构直接相连,天线连接段结构按照正四边形排布;天线连接段结构与对称振子使用等直径相同金属材料。振子互连对称振子阵列天线结构示意图的主视图、俯视图和立体图如图1、2和10所示。3) The structure of the antenna connection section is that the upper half of the four symmetrical vibrator structures are directly connected using the antenna connection section structure, and the lower half is directly connected using the same antenna connection section structure. The antenna connection section structure is arranged in a regular quadrilateral; the antenna connection section The structure and the symmetrical vibrator use the same metal material with the same diameter. The front view, top view and perspective view of the structural diagram of the symmetric dipole array antenna interconnected by dipoles are shown in Figures 1, 2 and 10.
4)在一定参数范围内,应用基于有源单元的电磁仿真来扫描参数搜寻最优的天线连接段结构与馈电点之间的距离ρh,而对称振子上、下两部分天线连接段结构间隔距离是天线连接段结构与馈电点之间的距离的两倍,即为2×ρh。得到如图3所示为直径0.1λ的四单元对称振子圆环阵S11参数随天线连接段结构与馈电点之间的距离的ρh的变化。可以得出与直线阵一样,对称振子天线连接段结构与馈电点之间的距离越大,天线单元的端口谐振特性越向高频处偏移,且谐振特性越差。在整个观察的频率范围内,S11参数整体下降比较明显。如图4和5中分别是直径0.1λ的四单元对称振子圆环阵天线单元1的幅度和相位方向图随对称振天线连接段结构与馈电点之间的距离ρh的变化,可以看出幅度和相位随对称振子天线连接段结构与馈电点之间的距离ρh的变化很大,但二者的变化趋势是一致,随着对称振子天线连接段结构与馈电点之间的距离ρh的增大,幅度和相位的变化越来越缓慢。天线单元1的最大辐射方向为,验证了天线单元之间的电磁耦合很强,能量主要被电磁耦合到其他的单元方向上。由上可知最优对称振子天线连接段结构与馈电点之间的距离为ρh=3mm,即对称阵子上、下两部分天线连接段结构间隔距离度2×ρh=6mm。4) Within a certain parameter range, the electromagnetic simulation based on the active unit is used to scan the parameters to search for the optimal distance ph between the antenna connecting section structure and the feeding point, and the distance between the upper and lower antenna connecting section structures of the symmetrical vibrator is The distance is twice the distance between the antenna connection section structure and the feed point, which is 2×ph. As shown in Figure 3, the change of the S 11 parameter of the four-element symmetrical oscillator circular array with a diameter of 0.1λ with the distance between the antenna connection section structure and the feeding point is obtained. It can be concluded that the same as the linear array, the greater the distance between the connecting section structure of the symmetrical dipole antenna and the feeding point, the more the port resonance characteristics of the antenna unit will shift to high frequencies, and the resonance characteristics will be worse. In the entire observed frequency range, the overall decrease of S 11 parameters is more obvious. As shown in Figures 4 and 5, the amplitude and phase patterns of the four-element symmetrical vibrator circular array antenna unit 1 with a diameter of 0.1λ vary with the distance ph between the connecting section structure of the symmetrical vibrating antenna and the feeding point. It can be seen that The amplitude and phase vary greatly with the distance ph between the connecting section structure of the symmetrical dipole antenna and the feeding point, but the trend of the two changes is consistent. The amplitude and phase changes more and more slowly. The maximum radiation direction of the antenna unit 1 is , which verifies that the electromagnetic coupling between the antenna units is very strong, and the energy is mainly electromagnetically coupled to other unit directions. It can be seen from the above that the distance between the optimal symmetrical dipole antenna connection section structure and the feed point is ph=3mm, that is, the distance between the upper and lower antenna connection section structures of the symmetrical element is 2×ph=6mm.
5)与传统非直连四单元对称振子相比,可以得到图6,即考虑电磁耦合的直连四单元对称振子圆环阵同考虑电磁耦合未直连的同参数天线阵的S参数比较图。考虑到阵列的对称性,这里只讨论天线单元1、天线单元2和天线单元3之间的相互作用。如图6所示,在工作频率1GHz处,天线的单元的S31小于-10dB,阵列单元的阻抗匹配特性相对于非直连的情况更好。而S21约为-8dB,S31小于-15dB,说明相邻天线端口之间存在一定程度的能量电磁耦合,但非相邻单元之间的能量电磁耦合并不明显。5) Compared with the traditional non-directly connected four-unit symmetrical oscillator, Figure 6 can be obtained, that is, the S-parameter comparison diagram of the direct-connected four-unit symmetrical oscillator circular array considering electromagnetic coupling and the same parameter antenna array not directly connected considering electromagnetic coupling . Considering the symmetry of the array, only the interaction between antenna unit 1, antenna unit 2 and antenna unit 3 is discussed here. As shown in FIG. 6 , at a working frequency of 1 GHz, the S 31 of the antenna elements is less than -10 dB, and the impedance matching characteristics of the array elements are better than those of non-direct connections. However, S 21 is about -8dB, and S 31 is less than -15dB, indicating that there is a certain degree of energy electromagnetic coupling between adjacent antenna ports, but the energy electromagnetic coupling between non-adjacent units is not obvious.
6)与传统非直连四单元对称振子相比,可以得到图7,即四单元电小间距直连对称振子阵列天线单元1的实际增益。可知,直连对称振子阵列的增益相对于非直连情况相比有明显增强,天线单元的实际增益提高了约5dB,且方向性更强,增益的变化更剧烈。6) Compared with the traditional non-directly connected four-element symmetric dipole, Figure 7 can be obtained, that is, the actual gain of the four-element direct-connected symmetric dipole array antenna unit 1 with small electrical spacing. It can be seen that the gain of the directly connected symmetric dipole array is significantly enhanced compared with the non-directly connected situation, and the actual gain of the antenna unit is increased by about 5dB, and the directivity is stronger, and the change of the gain is more drastic.
7)与传统非直连四单元对称振子相比,可以得到如图8所示的四单元电小间距直连对称振子阵列天线相位差变化。其中,Φ21表示单元天线单元1与天线单元2之间的相位差,Φ31表示单元天线单元1与天线单元3之间的相位差。非直连电磁耦合时,单元天线单元1与天线单元2之间的相位差变化范围是90°,而直连电磁耦合时,单元天线单元1与天线单元2之间的相位差变化范围是140°。非直连电磁耦合时,单元天线单元1与天线单元3之间的相位差变化范围是124°,而直连电磁耦合时,单元天线单元1与天线单元3之间的相位差变化范围是150°。可以得出直连电磁耦合比非直连情况天线阵元之间的相位差更大,提高了整个天线阵列对于目标信号来波方向敏感度。7) Compared with the traditional non-directly connected four-element symmetric dipole, the phase difference change of the four-element electrically small-pitch direct-connected symmetric dipole array antenna can be obtained as shown in FIG. 8 . Wherein, Φ 21 represents the phase difference between the unit antenna unit 1 and the antenna unit 2, and Φ 31 represents the phase difference between the unit antenna unit 1 and the antenna unit 3. In the case of indirect electromagnetic coupling, the range of phase difference between unit antenna unit 1 and antenna unit 2 is 90°, while in the case of direct electromagnetic coupling, the range of phase difference between unit antenna unit 1 and antenna unit 2 is 140° °. In the case of indirect electromagnetic coupling, the range of phase difference between unit antenna unit 1 and antenna unit 3 is 124°, while in the case of direct electromagnetic coupling, the range of phase difference between unit antenna unit 1 and antenna unit 3 is 150° °. It can be concluded that the direct electromagnetic coupling has a larger phase difference between the antenna elements than the non-direct connection, which improves the sensitivity of the entire antenna array to the incoming wave direction of the target signal.
8)与传统非直连四单元对称振子相比,可以得到如图9所示为四单元电小间距来波到达角方向估计的克拉美罗界和利用多重信号分类算法(Multiple SignalClassification Method,MUSIC)来波到达角方向估计的均方差。可知,整个方位角的变化范围内,直径为0.1λ四单元直连对称振子圆环阵的CRB和利用MUSIC算法进行来波到达角方向估计的均方差远低于非直连情况,这是由于电小间距四单元对称振子阵列的天线的对称性导致的。非直连电磁耦合情况下,阵列的测向精度为0.38°。而直连电磁耦合四单元圆环阵在整个观测角范围内,阵列的测向精度为0.25°,表明天线阵列的测向精度提高了。8) Compared with the traditional non-directly connected four-unit symmetric oscillator, the Cramereau boundary for the estimation of the arrival angle direction of the four-unit electrically small spacing can be obtained as shown in Figure 9 and the multiple signal classification algorithm (Multiple Signal Classification Method, MUSIC ) The mean square error of the incoming wave arrival angle direction estimate. It can be seen that within the entire range of azimuth angle variation, the mean square error of the CRB with a diameter of 0.1λ four-element direct-connected symmetrical oscillator circular array and the direction estimation of the incoming wave arrival angle using the MUSIC algorithm is much lower than that of the non-directly connected case. It is caused by the symmetry of the antenna of the four-element symmetric dipole array with electrically small spacing. In the case of indirect electromagnetic coupling, the direction finding accuracy of the array is 0.38°. In contrast, the direction-finding accuracy of the direct-connected electromagnetically coupled four-element circular array is 0.25° within the entire observation angle range, which indicates that the direction-finding accuracy of the antenna array has been improved.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611200989.6A CN106450709B (en) | 2016-12-22 | 2016-12-22 | Four-unit interconnected symmetrical oscillator circular antenna array for electric small-distance direction finding |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611200989.6A CN106450709B (en) | 2016-12-22 | 2016-12-22 | Four-unit interconnected symmetrical oscillator circular antenna array for electric small-distance direction finding |
Publications (2)
Publication Number | Publication Date |
---|---|
CN106450709A CN106450709A (en) | 2017-02-22 |
CN106450709B true CN106450709B (en) | 2019-12-06 |
Family
ID=58215230
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201611200989.6A Expired - Fee Related CN106450709B (en) | 2016-12-22 | 2016-12-22 | Four-unit interconnected symmetrical oscillator circular antenna array for electric small-distance direction finding |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106450709B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112380657A (en) * | 2020-12-01 | 2021-02-19 | 厦门大学 | Directional diagram synthesis method and device of circular ring array antenna |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2581444A (en) * | 1949-09-28 | 1952-01-08 | Standard Telephones Cables Ltd | Direction finder |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8866691B2 (en) * | 2007-04-20 | 2014-10-21 | Skycross, Inc. | Multimode antenna structure |
-
2016
- 2016-12-22 CN CN201611200989.6A patent/CN106450709B/en not_active Expired - Fee Related
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2581444A (en) * | 1949-09-28 | 1952-01-08 | Standard Telephones Cables Ltd | Direction finder |
Non-Patent Citations (1)
Title |
---|
《Investigation of wideband Coaxial-Fed Circular dipole Array antenna in a Borehole》;Satoshi Ebihara et-al;《2011 6th International Workshop on Advanced Ground Penetrating Radar (IWAGPR)》;20010729;第1-5页 * |
Also Published As
Publication number | Publication date |
---|---|
CN106450709A (en) | 2017-02-22 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105226400B (en) | A broadband dual-polarized phased array antenna and full-polarization beamforming method | |
CN106654564B (en) | Phase Interferometer and Its Parameter Estimation Method Based on Broadband Conformal Antenna Array | |
CN102280687B (en) | High-isolation four-port diversity antenna for mobile communication | |
CN106848546B (en) | A broadband dual-polarized antenna array device and high-resolution direction finding method | |
CN106483494B (en) | A Fully Polarized Interferometer Based on Spatially Sampling Antenna Array and Its Parameter Estimation Method | |
CN102544724B (en) | Dual-polarized single pulse broadband microstrip antenna device | |
CN106450714A (en) | Broadband circularly-polarized antenna applicable to arrays | |
CN104882672A (en) | Wide bandwidth wave beam circular polarization Yagi-microstrip antenna | |
CN106654507B (en) | The direction-finding method of phase-interferometer based on broadband dual polarized antenna array | |
CN213093358U (en) | A circularly polarized FP resonant cavity antenna | |
WO2019100376A1 (en) | Omnidirectional array antenna and beamforming method therefor | |
CN102983401A (en) | Low-consumption low-minor lobe high-gain planar frequency scan antenna | |
CN115579649A (en) | Two-dimensional wide-angle scanning programmable bit array antenna with low cost and low profile | |
CN114221109A (en) | A broadband high-gain magnetoelectric dipole transmission array antenna unit and transmission array antenna | |
CN106486756B (en) | A Broadband Low Profile Pattern Reconfigurable Antenna | |
CN106450709B (en) | Four-unit interconnected symmetrical oscillator circular antenna array for electric small-distance direction finding | |
CN209298340U (en) | Miniaturized Wide Bandwidth Beam Circularly Polarized Microstrip Antenna for C-Band | |
CN104362437A (en) | S-frequency-band monopulse self-tracking antenna system | |
CN102377020A (en) | Dual-frequency microstrip patch antenna for high-precision measurement | |
CN216120772U (en) | Circularly polarized PSOAM array antenna and wireless communication system | |
CN108011183B (en) | One-dimensional wide angle based on rectangular patch TM20 mode scans phased array | |
CN105811117A (en) | Multi-beam radiation and polarization regulation design method based on anisotropic electromagnetic metasurface | |
CN109361068B (en) | Polarization converter for orthogonally deflecting polarization of electromagnetic wave in any direction | |
Rao et al. | A shared-aperture dual-band sub-6 GHz and mmWave reconfigurable intelligent surface with independent operation | |
CN116865001A (en) | One-dimensional wide-angle scanning phased array antenna based on multiple modes |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
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: 20191206 |