[go: up one dir, main page]

CN102709675A - Antenna for satellite communication in motion - Google Patents

Antenna for satellite communication in motion Download PDF

Info

Publication number
CN102709675A
CN102709675A CN2012101329731A CN201210132973A CN102709675A CN 102709675 A CN102709675 A CN 102709675A CN 2012101329731 A CN2012101329731 A CN 2012101329731A CN 201210132973 A CN201210132973 A CN 201210132973A CN 102709675 A CN102709675 A CN 102709675A
Authority
CN
China
Prior art keywords
metal
impedance matching
core layer
metamaterial
substrate
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
CN2012101329731A
Other languages
Chinese (zh)
Other versions
CN102709675B (en
Inventor
刘若鹏
季春霖
李星昆
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.)
Kuang-Chi Institute of Advanced Technology
Original Assignee
Kuang Chi Innovative Technology Ltd
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 Kuang Chi Innovative Technology Ltd filed Critical Kuang Chi Innovative Technology Ltd
Priority to CN201210132973.1A priority Critical patent/CN102709675B/en
Publication of CN102709675A publication Critical patent/CN102709675A/en
Application granted granted Critical
Publication of CN102709675B publication Critical patent/CN102709675B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Aerials With Secondary Devices (AREA)

Abstract

本发明公开了一种动中通天线,包括两个相同的方形超材料平板及设置在两个超材料平板之间的馈源,两个超材料平板的上边缘固定连接,馈源等效点在两个超材料平板上的投影与两个超材料平板的表面中心点重合,每一超材料平板包括核心层,核心层包括一个核心层片层或多个相同的核心层片层,每一核心层片层包括片状的第一基材及设置在第一基材上的多个第一人造微结构,通过精确设计核心层片层的折射率分布,使得由馈源发出的电磁波经超材料平板后能以平面波的形式出射,或者是从卫星上发来的垂直入射的平面波经超材料平板后能够在馈源处汇聚。本发明的动中通天线,由两个片状的超材料平板组合代替传统的抛物面天线,制造加工容易,成本低廉。

Figure 201210132973

The invention discloses a communication antenna in motion, which comprises two identical square metamaterial plates and a feed source arranged between the two metamaterial plates, the upper edges of the two metamaterial plates are fixedly connected, and the equivalent point of the feed source is The projection on the two metamaterial flat plates coincides with the surface centers of the two metamaterial flat plates, each metamaterial flat plate includes a core layer, and the core layer includes a core layer sheet or a plurality of identical core layer sheets, each The core layer sheet includes a sheet-shaped first substrate and a plurality of first artificial microstructures arranged on the first substrate. By precisely designing the refractive index distribution of the core layer sheet, the electromagnetic wave emitted by the feed source passes through the ultra- The material slab can exit in the form of plane waves, or the vertically incident plane waves sent from the satellite can converge at the feed source after passing through the metamaterial slab. The mobile communication antenna of the present invention replaces the traditional parabolic antenna by combining two sheet-like metamaterial flat plates, which is easy to manufacture and process, and has low cost.

Figure 201210132973

Description

一种动中通天线An antenna in motion

技术领域 technical field

本发明涉及通信领域,更具体地说,涉及一种动中通天线。The present invention relates to the communication field, and more specifically, relates to a mobile communication antenna.

背景技术 Background technique

动中通是“移动中的卫星地面站通信系统”的简称。通过动中通系统,车辆、轮船、飞机等移动的载体在运动过程中可实时跟踪卫星等平台,不间断地传递语音、数据、图像等多媒体信息,可满足各种军民用应急通信和移动条件下的多媒体通信的需要。动中通系统很好地解决了各种车辆、轮船等移动载体在运动中通过地球同步卫星,实时不断地传递语音、数据、高清晰的动态视频图像、传真等多媒体信息的难关,是通信领域的一次重大的突破,是当前卫星通信领域需求旺盛、发展迅速的应用领域,在军民两个领域都有极为广泛的发展前景。Mobile Communication is the abbreviation of "Moving Satellite Ground Station Communication System". Through the mobile communication system, vehicles, ships, aircraft and other mobile carriers can track satellites and other platforms in real time during the movement process, and continuously transmit multimedia information such as voice, data, images, etc., which can meet various military and civilian emergency communication and mobile conditions Under the needs of multimedia communication. The mobile communication system solves the problem that various vehicles, ships and other mobile carriers transmit voice, data, high-definition dynamic video images, faxes and other multimedia information in real time through geosynchronous satellites in motion. It is a major breakthrough in the current satellite communication field, which has a strong demand and a fast-growing application field, and has extremely broad development prospects in both military and civilian fields.

作为动中通系统的一个重要组成部分,动中通天线负责通信信号的接收和/或发送,传统的动中通天线一般采用抛物面天线。As an important part of the mobile communication system, the mobile communication antenna is responsible for the reception and/or transmission of communication signals. Traditional mobile communication antennas generally use parabolic antennas.

但是由于抛物面天线的反射面的曲面加工难度大,精度要求也高,因此,制造麻烦,且成本较高。However, since the curved surface of the reflective surface of the parabolic antenna is difficult to process and requires high precision, the manufacturing is troublesome and the cost is relatively high.

发明内容 Contents of the invention

本发明所要解决的技术问题是,针对现有的动中通天线加工不易、成本高的缺陷,提供一种加工简单、制造成本低的动中通天线。The technical problem to be solved by the present invention is to provide a mobile communication antenna with simple processing and low manufacturing cost in view of the defects of difficult processing and high cost of the existing mobile communication antennas.

本发明解决其技术问题所采用的技术方案是:一种动中通天线,所述动中通天线包括两个相同的方形超材料平板及设置在两个超材料平板之间的馈源,所述两个超材料平板的上边缘固定连接,馈源等效点在两个超材料平板上的投影与两个超材料平板的表面中心点重合,在伺服系统的控制下,所述馈源的开口始终正对更靠近通信卫星的那个超材料平板,所述两个超材料平板具有相同的折射率分布规律,每一超材料平板包括核心层,所述核心层包括一个核心层片层或多个相同的核心层片层,每一个核心层片层包括片状的第一基材以及设置在第一基材上的多个第一人造微结构,任一核心层片层的折射率分布满足如下公式:The technical solution adopted by the present invention to solve the technical problem is: a communication antenna in motion, which includes two identical square metamaterial flat plates and a feed source arranged between the two metamaterial flat plates. The upper edges of the two metamaterial slabs are fixedly connected, and the projection of the equivalent point of the feed source on the two metamaterial slabs coincides with the center point of the surface of the two metamaterial slabs. Under the control of the servo system, the feed source The opening is always facing the metamaterial slab that is closer to the communication satellite, and the two metamaterial slabs have the same refractive index distribution law, and each metamaterial slab includes a core layer, and the core layer includes one core layer sheet or more The same core layer sheet, each core layer sheet includes a sheet-shaped first substrate and a plurality of first artificial microstructures arranged on the first substrate, and the refractive index distribution of any core layer sheet satisfies The following formula:

nno (( rr )) == nno maxmax -- rr 22 ++ sthe s 22 -- VsegVseg DD. ;;

Vseg=s+λ×NUMseg;Vseg=s+λ×NUMseg;

NUMsegNUMseg == floorfloor {{ rr 22 ++ sthe s 22 -- sthe s λλ }} ;;

DD. == λλ nno maxmax -- nno minmin ;;

其中,n(r)表示该核心层片层上半径为r处的折射率值,核心层片层的折射率分布圆心即为馈源等效点在该核心层片层表面的投影;Wherein, n(r) represents the refractive index value at the radius of r on the core layer sheet, and the center of the refractive index distribution circle of the core layer sheet is the projection of the equivalent point of the feed source on the surface of the core layer sheet;

s为馈源等效点到超材料平板的垂直距离;s is the vertical distance from the feed equivalent point to the metamaterial plate;

nmax表示核心层片层的折射率的最大值;n max represents the maximum value of the refractive index of the core layer sheet;

nmin表示核心层片层的折射率的最小值;n min represents the minimum value of the refractive index of the core layer sheet;

D为超材料平板的整体厚度;D is the overall thickness of the metamaterial slab;

λ表示频率为天线中心频率的电磁波的波长;λ represents the wavelength of the electromagnetic wave whose frequency is the center frequency of the antenna;

floor表示向下取整;floor means rounding down;

其中,两个超材料平板之间的夹角为θ,Among them, the angle between two metamaterial plates is θ,

tgtg θθ 22 == 22 sthe s LL ;;

L表示方形超材料平板构成θ夹角的两个边的长度。L represents the length of the two sides forming the included angle θ of the square metamaterial flat plate.

进一步地,所述第一基材包括片状的第一前基板及第一后基板,所述多个第一人造微结构夹设在第一前基板与第一后基板之间,所述核心层片层的厚度为0.21-2.5mm,其中,第一前基板的厚度为0.1-1mm,第一后基板的厚度为0.1-1mm,多个第一人造微结构的厚度为0.01-0.5mm。Further, the first substrate includes a sheet-shaped first front substrate and a first rear substrate, the plurality of first artificial microstructures are sandwiched between the first front substrate and the first rear substrate, and the core The thickness of the ply layer is 0.21-2.5mm, wherein the thickness of the first front substrate is 0.1-1mm, the thickness of the first rear substrate is 0.1-1mm, and the thickness of the plurality of first artificial microstructures is 0.01-0.5mm.

进一步地,所述核心层片层的厚度为0.543mm,其中,第一前基板及第一后基板的厚度均为0.254mm,多个第一人造微结构的厚度为0.035mm。Further, the thickness of the core layer is 0.543 mm, wherein the thickness of the first front substrate and the first rear substrate are both 0.254 mm, and the thickness of the plurality of first artificial microstructures is 0.035 mm.

进一步地,每一超材料平板还包括设置在核心层两侧表面的阻抗匹配层,所述阻抗匹配层包括一个阻抗匹配层片层或多个厚度相同的阻抗匹配层片层,所述阻抗匹配层片层包括片状的第二基材以及设置在第二基材上的多个第二人造微结构,所述一个或多个阻抗匹配层片层的折射率分布满足如下公式:Further, each metamaterial slab also includes impedance matching layers arranged on both sides of the core layer. The impedance matching layer includes one impedance matching layer sheet or a plurality of impedance matching layer sheets with the same thickness. The impedance matching layer The layer includes a sheet-shaped second substrate and a plurality of second artificial microstructures disposed on the second substrate, and the refractive index distribution of the one or more impedance matching layers satisfies the following formula:

nno ii (( rr )) == nno minmin ii mm ×× nno (( rr )) mm -- ii mm ;;

其中,ni(r)表示阻抗匹配层片层上半径为r处的折射率值,阻抗匹配层片层的折射率分布圆心即为馈源等效点在相应的阻抗匹配层片层外侧表面所在平面的投影;Among them, n i (r) represents the refractive index value at the radius r on the impedance matching layer, and the center of the refractive index distribution circle of the impedance matching layer is the equivalent point of the feed source on the outer surface of the corresponding impedance matching layer The projection of the plane on which it is located;

其中,i表示阻抗匹配层片层的编号,靠近核心层的阻抗匹配层片层的编号为1,两边最外侧的阻抗匹配层片层的编号为m,由核心层向两侧方向,编号依次减小;Among them, i represents the number of the impedance matching layer. The number of the impedance matching layer near the core layer is 1, and the number of the outermost impedance matching layer on both sides is m. From the core layer to the two sides, the numbers are sequential. decrease;

上述的nmax、nmin分别与核心层片层的折射率的最大值、最小值相同。The aforementioned n max and n min are respectively the same as the maximum and minimum values of the refractive index of the core layer sheet.

进一步地,每一超材料平板还包括设置在核心层两侧表面的阻抗匹配层,所述阻抗匹配层包括一个阻抗匹配层片层或多个厚度相同的阻抗匹配层片层,所述阻抗匹配层片层包括片状的第二基材以及设置在第二基材上的多个第二人造微结构,所述每一阻抗匹配层片层具有单一的折射率,所述一个或多个阻抗匹配层片层的折射率满足以下公式:Further, each metamaterial slab also includes impedance matching layers arranged on both sides of the core layer. The impedance matching layer includes one impedance matching layer sheet or a plurality of impedance matching layer sheets with the same thickness. The impedance matching layer The layer includes a sheet-shaped second substrate and a plurality of second artificial microstructures disposed on the second substrate, each of the impedance matching layers has a single refractive index, and the one or more impedance The refractive index of the matching layer satisfies the following formula:

nno (( ii )) == (( (( nno maxmax ++ nno minmin )) // 22 )) ii mm ;;

其中,m表示阻抗匹配层的总层数,i表示阻抗匹配层片层的编号,其中,靠近核心层的阻抗匹配层片层的编号为m,由核心层向两侧方向,编号依次减小,两边最外侧的阻抗匹配层片层的编号为1。Among them, m represents the total number of layers of the impedance matching layer, and i represents the number of the impedance matching layer, wherein the number of the impedance matching layer near the core layer is m, and the number decreases in turn from the core layer to both sides. , the number of the outermost impedance matching layer on both sides is 1.

进一步地,所述第二基材包括片状的第二前基板及第二后基板,所述多个第二人造微结构夹设在第二前基板与第二后基板之间,所述阻抗匹配层片层的厚度为0.21-2.5mm,其中,第二前基板的厚度为0.1-1mm,第二后基板的厚度为0.1-1mm,多个第二人造微结构的厚度为0.01-0.5mm。Further, the second substrate includes a sheet-shaped second front substrate and a second rear substrate, the plurality of second artificial microstructures are interposed between the second front substrate and the second rear substrate, and the impedance The thickness of the matching layer is 0.21-2.5mm, wherein the thickness of the second front substrate is 0.1-1mm, the thickness of the second rear substrate is 0.1-1mm, and the thickness of the plurality of second artificial microstructures is 0.01-0.5mm .

进一步地,所述第一人造微结构及第二人造微结构均为由铜线或银线构成的金属微结构,所述金属微结构通过蚀刻、电镀、钻刻、光刻、电子刻或离子刻的方法分别附着在第一基材及第二基材上。Further, both the first artificial microstructure and the second artificial microstructure are metal microstructures composed of copper wires or silver wires, and the metal microstructures are formed by etching, electroplating, drilling, photolithography, electronic engraving or ionization. The method of engraving is respectively attached to the first base material and the second base material.

进一步地,所述金属微结构呈平面雪花状,所述金属微结构具有相互垂直平分的第一金属线及第二金属线,所述第一金属线与第二金属线的长度相同,所述第一金属线两端连接有相同长度的两个第一金属分支,所述第一金属线两端连接在两个第一金属分支的中点上,所述第二金属线两端连接有相同长度的两个第二金属分支,所述第二金属线两端连接在两个第二金属分支的中点上,所述第一金属分支与第二金属分支的长度相等。Further, the metal microstructure is in the shape of a plane snowflake, the metal microstructure has a first metal line and a second metal line that are perpendicular to each other, and the length of the first metal line is the same as that of the second metal line. Two first metal branches of the same length are connected at both ends of the first metal line, the two ends of the first metal line are connected at the midpoint of the two first metal branches, and the two ends of the second metal line are connected with the same Two second metal branches of the same length, the two ends of the second metal wire are connected to the midpoint of the two second metal branches, and the length of the first metal branch is equal to that of the second metal branch.

进一步地,所述平面雪花状的金属微结构的每个第一金属分支及每个第二金属分支的两端还连接有完全相同的第三金属分支,相应的第三金属分支的中点分别与第一金属分支及第二金属分支的端点相连。Further, the two ends of each first metal branch and each second metal branch of the planar snowflake-shaped metal microstructure are also connected to identical third metal branches, and the midpoints of the corresponding third metal branches are respectively It is connected with the terminals of the first metal branch and the second metal branch.

进一步地,所述平面雪花状的金属微结构的第一金属线与第二金属线均设置有两个弯折部,所述平面雪花状的金属微结构绕第一金属线与第二金属线的交点在金属微结构所处平面内向任意方向旋转90度的图形都与原图重合。Further, the first metal wire and the second metal wire of the planar snowflake-shaped metal microstructure are both provided with two bending parts, and the planar snowflake-shaped metal microstructure wraps around the first metal wire and the second metal wire The graphs of the intersection points rotated 90 degrees in any direction in the plane where the metal microstructure is located coincide with the original graph.

根据本发明的动中通天线,通过精确设计每一块超材料平板的折射率分布,使得特定角度的平面波经超材料平板中空结构后能够在馈源处汇聚,因此可以由五个片状的超材料平板组合代替了传统的抛物面天线,制造加工更加容易,成本更加低廉,另外依此设计的超材料平板整体厚度在毫米级别,该动中通天线整体较轻。According to the mobile communication antenna of the present invention, by precisely designing the refractive index distribution of each metamaterial slab, the plane wave at a specific angle can be converged at the feed source after passing through the hollow structure of the metamaterial slab. The material plate combination replaces the traditional parabolic antenna, which is easier to manufacture and process, and the cost is lower. In addition, the overall thickness of the metamaterial plate designed based on this is at the millimeter level, and the overall communication antenna is lighter.

附图说明 Description of drawings

图1是本发明一种实施例中超材料平板与其对应的馈源的相对位置示意图;Fig. 1 is a schematic diagram of the relative position of a metamaterial plate and its corresponding feed source in an embodiment of the present invention;

图2是本发明的核心层片层其中一个超材料单元的透视示意图;Fig. 2 is a schematic perspective view of one of the metamaterial units in the core layer of the present invention;

图3是本发明的核心层片层的结构示意图;Fig. 3 is a schematic structural view of the core layer sheet of the present invention;

图4是本发明的阻抗匹配层片层的结构示意图;Fig. 4 is a schematic structural view of the impedance matching layer of the present invention;

图5是本发明的平面雪花状的金属微结构的示意图;Fig. 5 is the schematic diagram of the metal microstructure of plane snowflake shape of the present invention;

图6是图5所示的平面雪花状的金属微结构的一种衍生结构;Fig. 6 is a kind of derivation structure of the metal microstructure of plane snowflake shape shown in Fig. 5;

图7是图5所示的平面雪花状的金属微结构的一种变形结构。FIG. 7 is a deformed structure of the planar snowflake-shaped metal microstructure shown in FIG. 5 .

图8是平面雪花状的金属微结构的拓扑形状的演变的第一阶段;Figure 8 is the first stage of the evolution of the topological shape of the planar snowflake-like metal microstructure;

图9是平面雪花状的金属微结构的拓扑形状的演变的第二阶段;Figure 9 is the second stage of the evolution of the topological shape of the planar snowflake-like metal microstructure;

图10是本发明另一种实施例中超材料平板与其对应的馈源的相对位置示意图;Fig. 10 is a schematic diagram of the relative position of the metamaterial plate and its corresponding feed source in another embodiment of the present invention;

图11是本发明动中通天线的结构示意图;Fig. 11 is a schematic structural diagram of the antenna in motion of the present invention;

图12是本发明动中通天线在车辆上的安装结构示意图;Fig. 12 is a schematic diagram of the installation structure of the mobile communication antenna on the vehicle according to the present invention;

图13表示图12所示的动中通天线其过馈源中轴线的截面示意图。FIG. 13 is a schematic cross-sectional view of the antenna in motion shown in FIG. 12 passing through the central axis of the feed source.

具体实施方式 Detailed ways

如图1、图11及图12所示,本发明的所述动中通天线DZT装载在移动载体YDT(例如车辆、船舶、飞机)的顶部位置,其包括两个相同的方形超材料平板100及设置在两个超材料平板100之间的馈源1,所述两个超材料平板100的上边缘固定连接,馈源等效点X在两个超材料平板上的投影与两个超材料平板的表面中心点重合,如图11所示,即馈源等效点X在超材料平板101上的投影与超材料平板101的表面中心点O1重合,馈源等效点X在超材料平板102上的投影与超材料平板102的表面中心点O2重合,在伺服系统CF的控制下,所述馈源1的开口始终正对更靠近通信卫星的那个超材料平板。本发明中,所述馈源1为传统的波纹喇叭,例如同洲电子的CL11R一体化高频头。As shown in Fig. 1, Fig. 11 and Fig. 12, the communication-in-motion antenna DZT of the present invention is loaded on the top position of the mobile carrier YDT (such as vehicle, ship, aircraft), which includes two identical square metamaterial flat plates 100 And the feed source 1 arranged between two metamaterial flat panels 100, the upper edges of the two metamaterial flat panels 100 are fixedly connected, the projection of the feed source equivalent point X on the two metamaterial flat panels is the same as the two metamaterial flat panels The center point of the surface of the plate coincides, as shown in Figure 11, that is, the projection of the feed source equivalent point X on the metamaterial plate 101 coincides with the surface center point O1 of the metamaterial plate 101, and the feed source equivalent point X is on the metamaterial plate 101. The projection on 102 coincides with the surface center point O2 of the metamaterial slab 102, and under the control of the servo system CF, the opening of the feed 1 is always facing the metamaterial slab closer to the communication satellite. In the present invention, the feed source 1 is a traditional corrugated horn, such as the CL11R integrated tuner of Coship Electronics.

伺服系统CF的功用如下:The functions of the servo system CF are as follows:

(1)调节两个超材料平板的在三维空间中的旋转,即调节动中通天线的仰角与方位角,使得所要通信的卫星天线发出的电磁波到达动中通天线处时总是与其中一个超材料平板垂直;(1) Adjust the rotation of the two metamaterial plates in three-dimensional space, that is, adjust the elevation angle and azimuth angle of the mobile communication antenna, so that the electromagnetic wave emitted by the satellite antenna to be communicated always coincides with one of the mobile communication antennas when it reaches the mobile communication antenna. metamaterial slab vertical;

(2)实现馈源三维扫描,使得所述馈源的开口始终正对更靠近通信卫星的那个超材料平板,即馈源中轴线Z1经过超材料平板101的表面中心点O1或超材料平板102的表面中心点O2。(2) Realize the three-dimensional scanning of the feed source, so that the opening of the feed source is always facing the metamaterial flat plate closer to the communication satellite, that is, the central axis Z1 of the feed source passes through the surface center point O1 of the metamaterial flat plate 101 or the metamaterial flat plate 102 The center point O2 of the surface.

相对于只有一块超材料板的设计,设计两个超材料板可以使得动中通的反应更加灵敏,即动中通天线的方位角的调节不需要旋转太大的角度,只需要将靠近通信卫星的超材料平板对准卫星即可。Compared with the design of only one metamaterial board, the design of two metamaterial boards can make the response of the mobile communication more sensitive, that is, the adjustment of the azimuth angle of the mobile communication antenna does not need to be rotated too much, and only needs to be close to the communication satellite. The metamaterial slab can be aligned with the satellite.

具有上述功能的伺服系统现有技术中已经存在很多,其不是本发明的核心,并且本领域的技术人员根据上述文字描述可以很容易地制作出具有类似功能的伺服系统,此处不再详述。There are many servo systems with the above functions in the prior art, which are not the core of the present invention, and those skilled in the art can easily make servo systems with similar functions according to the above text description, and will not be described in detail here .

另外,如图12所示,为了对动中通天线DZT进行保护(防水、防晒等),动中通天线的外部还可以罩一个天线罩TXZ,例如半球形的天线罩。In addition, as shown in FIG. 12 , in order to protect the mobile communication antenna DZT (waterproof, sun protection, etc.), the mobile communication antenna can also be covered with a radome TXZ, such as a hemispherical radome.

如图1至图4所示,本发明的一个实施例中,所述超材料平板100包括核心层10、设置在核心层两侧表面的阻抗匹配层20,优选地,所述两侧表面的阻抗匹配层20在核心层的两侧呈对称分布,所述核心层10包括一个核心层片层11或多个厚度相同且折射率分布相同的核心层片层11,所述核心层片层包括片状的第一基材13以及设置在第一基材13上的多个第一人造微结构12,所述阻抗匹配层20包括一个阻抗匹配层片层21或厚度相同的多个阻抗匹配层片层21,所述阻抗匹配层片层21包括片状的第二基材23以及设置在第二基材上的多个第二人造微结构。阻抗匹配层的作用是实现从空气到核心层10的阻抗匹配,以减少空气与超材料相接处的电磁波反射,降低电磁波能量的损失,提高卫星电视信号强度。As shown in Figures 1 to 4, in an embodiment of the present invention, the metamaterial slab 100 includes a core layer 10, impedance matching layers 20 disposed on both sides of the core layer, preferably, the two sides of the surface The impedance matching layer 20 is symmetrically distributed on both sides of the core layer, the core layer 10 includes a core layer sheet 11 or a plurality of core layer sheets 11 with the same thickness and the same refractive index distribution, and the core layer sheet includes A sheet-shaped first substrate 13 and a plurality of first artificial microstructures 12 disposed on the first substrate 13, the impedance matching layer 20 includes an impedance matching layer sheet 21 or a plurality of impedance matching layers with the same thickness Sheet 21, the impedance matching layer sheet 21 includes a sheet-shaped second substrate 23 and a plurality of second artificial microstructures disposed on the second substrate. The function of the impedance matching layer is to realize the impedance matching from the air to the core layer 10, so as to reduce the electromagnetic wave reflection at the junction between the air and the metamaterial, reduce the loss of electromagnetic wave energy, and improve the satellite TV signal strength.

本发明中,任一核心层片层的折射率分布满足如下公式:In the present invention, the refractive index distribution of any core layer sheet satisfies the following formula:

nno (( rr )) == nno maxmax -- rr 22 ++ sthe s 22 -- VsegVseg DD. -- -- -- (( 11 )) ;;

Vseg=s+λ×NUMseg  (2);Vseg=s+λ×NUMseg (2);

NUMsegNUMseg == floorfloor {{ rr 22 ++ sthe s 22 -- sthe s λλ }} -- -- -- (( 33 )) ;;

DD. == λλ nno maxmax -- nno minmin -- -- -- (( 44 )) ;;

其中,n(r)表示该核心层片层上半径为r处的折射率值,核心层片层的折射率分布圆心O即为馈源等效点X在该核心层片层表面的投影;同时,折射率分布圆心O也是该核心层片层的表面中心点。Wherein, n(r) represents the refractive index value at the radius r on the core layer sheet, and the refractive index distribution center O of the core layer sheet is the projection of the feed source equivalent point X on the surface of the core layer sheet; At the same time, the center O of the refractive index distribution is also the center point of the surface of the core layer sheet.

s为馈源等效点X到超材料平板的垂直距离;此处馈源的等效点X实际上就是天线的馈点(电磁波在馈源中发生聚焦的点);馈源等效点X在馈源的中轴线上,且馈源等效点X在距离馈源开口中心一定距离的位置上,此距离可以通过仿真或实测得到。s is the vertical distance from the feed equivalent point X to the metamaterial flat plate; the equivalent point X of the feed here is actually the feed point of the antenna (the point where the electromagnetic wave is focused in the feed); the equivalent point X of the feed is On the central axis of the feed source, and the equivalent point X of the feed source is at a certain distance from the center of the feed source opening. This distance can be obtained through simulation or actual measurement.

nmax表示核心层片层的折射率的最大值;n max represents the maximum value of the refractive index of the core layer sheet;

nmin表示核心层片层的折射率的最小值;n min represents the minimum value of the refractive index of the core layer sheet;

λ表示频率为天线中心频率的电磁波的波长;λ represents the wavelength of the electromagnetic wave whose frequency is the center frequency of the antenna;

D为超材料平板的整体厚度,本实施例中,即指核心层与阻抗匹配层的总厚度,核心层片层与阻抗匹配层片层的数量可以根据不同需要设定,例如,可以是四个核心层片层,两边各三个阻抗匹配层片层,也可是三个核心层片层,两边各两个阻抗匹配层片层;D is the overall thickness of the metamaterial flat plate. In this embodiment, it refers to the total thickness of the core layer and the impedance matching layer. The number of core layer sheets and impedance matching layer sheets can be set according to different needs. For example, it can be four A core layer sheet, three impedance matching layer sheets on both sides, or three core layer sheets, two impedance matching layer sheets on both sides;

floor表示向下取整,例如,当

Figure BDA0000159140260000071
(r处于某一数值范围)大于等于0小于1时,NUMseg取0,当
Figure BDA0000159140260000072
(r处于某一数值范围)大于等于1小于2时,NUMseg取1,依此类推。floor represents rounding down, for example, when
Figure BDA0000159140260000071
(r is in a certain value range) greater than or equal to 0 and less than 1, NUMseg takes 0, when
Figure BDA0000159140260000072
(r is in a certain value range) When it is greater than or equal to 1 and less than 2, NUMseg takes 1, and so on.

其中,如图13所示,表示图12所示的动中通天线其过馈源中轴线的截面示意图(当馈源开口正对超材料平板102时)。Wherein, as shown in FIG. 13 , it shows a schematic cross-sectional view of the antenna in motion shown in FIG. 12 passing through the central axis of the feed source (when the feed source opening faces the metamaterial flat plate 102 ).

从图中可以看出,两个超材料平板之间的夹角为θ,半角即为

Figure BDA0000159140260000073
由三角函数关系可得到:It can be seen from the figure that the angle between two metamaterial plates is θ, and the half angle is
Figure BDA0000159140260000073
From the trigonometric function relationship, we can get:

tgtg θθ 22 == 22 sthe s LL -- -- -- (( 55 )) ;;

L表示方形超材料平板构成θ夹角的两个边的长度。L represents the length of the two sides forming the included angle θ of the square metamaterial flat plate.

综上,可以看出,夹角θ由馈源等效点X到超材料平板的距离s以及方形超材料平板构成θ夹角的两个边的长度L共同决定。In summary, it can be seen that the angle θ is determined by the distance s from the equivalent point X of the feed source to the metamaterial plate and the length L of the two sides of the square metamaterial plate forming the angle θ.

由公式(1)至公式(4)所确定的超材料平板,能够使得馈源发出的电磁波经超材料平板后能够以平面波的形式出射;同样,如图1所示,由公式(1)至公式(4)所确定的超材料平板,能够使得卫星发出的电磁波(到达地面时可认为是平面波)经超材料平板后能够在馈源的等效点X处发生汇聚;当然,在接收卫星天线信号时,超材料平板的法线方向是朝向所要接收的卫星的,至于如何使得超材料平板的法线方向朝向所要接收信号的卫星,则涉及到传统的卫星天线调试的问题,即关于天线方位角与俯仰角的调节,其通过伺服系统均可以实现,其均为公知常识,此处不再述说。The metamaterial plate determined by formula (1) to formula (4) can make the electromagnetic wave emitted by the feed source exit in the form of a plane wave after passing through the metamaterial plate; similarly, as shown in Figure 1, from formula (1) to The metamaterial slab determined by formula (4) can make the electromagnetic waves emitted by the satellite (which can be regarded as plane waves when reaching the ground) converge at the equivalent point X of the feed source after passing through the metamaterial slab; of course, in the receiving satellite antenna When receiving a signal, the normal direction of the metamaterial slab faces the satellite to be received. As for how to make the normal direction of the metamaterial slab face the satellite to receive the signal, it involves the problem of traditional satellite antenna debugging, that is, the antenna orientation The adjustment of the angle and the pitch angle can be realized by the servo system, which is common knowledge and will not be described here.

本实施例中,如图3所示,所述第一基材13包括片状的第一前基板131及第一后基板132,所述多个第一人造微结构12夹设在第一前基板131与第一后基板132之间。所述核心层片层的厚度为0.5-2mm,其中,第一前基板的厚度为0.5-1mm,第一后基板的厚度为0.5-1mm,多个第一人造微结构的厚度为0.01-0.5mm。优选地,所述核心层片层的厚度为0.543mm,其中,第一前基板及第一后基板的厚度均为0.254mm,多个第一人造微结构的厚度为0.035mm。In this embodiment, as shown in FIG. 3 , the first substrate 13 includes a sheet-shaped first front substrate 131 and a first rear substrate 132, and the plurality of first artificial microstructures 12 are sandwiched between the first front substrate 131 and the first rear substrate 132. between the substrate 131 and the first rear substrate 132 . The thickness of the core layer sheet is 0.5-2mm, wherein the thickness of the first front substrate is 0.5-1mm, the thickness of the first rear substrate is 0.5-1mm, and the thickness of the plurality of first artificial microstructures is 0.01-0.5 mm. Preferably, the core layer has a thickness of 0.543mm, wherein the first front substrate and the first rear substrate both have a thickness of 0.254mm, and the plurality of first artificial microstructures have a thickness of 0.035mm.

本实施例中,所述一个或多个阻抗匹配层片层的折射率分布满足如下公式:In this embodiment, the refractive index distribution of the one or more impedance matching layers satisfies the following formula:

nno ii (( rr )) == nno minmin ii mm ×× nno (( rr )) mm -- ii mm -- -- -- (( 55 )) ;;

其中,ni(r)表示阻抗匹配层片层上半径为r处的折射率值,阻抗匹配层片层的折射率分布圆心即为馈源等效点在相应的阻抗匹配层片层外侧表面所在平面的投影,优选地,阻抗匹配层片层的折射率分布圆心与核心层片层的折射率分布圆心的连线垂直超材料平板;Among them, n i (r) represents the refractive index value at the radius r on the impedance matching layer, and the center of the refractive index distribution circle of the impedance matching layer is the equivalent point of the feed source on the outer surface of the corresponding impedance matching layer The projection of the plane where it is located, preferably, the line between the center of the refractive index distribution of the impedance matching layer and the center of the refractive index distribution of the core layer is a vertical metamaterial flat plate;

其中,i表示阻抗匹配层片层的编号,靠近核心层的阻抗匹配层片层的编号为1,两边最外侧的阻抗匹配层片层的编号为m,由核心层向两侧方向,编号依次减小;Among them, i represents the number of the impedance matching layer. The number of the impedance matching layer near the core layer is 1, and the number of the outermost impedance matching layer on both sides is m. From the core layer to the two sides, the numbers are sequential. decrease;

此处的n(r)表示核心层片层上半径为r处的折射率值;Here n(r) represents the refractive index value at the radius r on the core layer sheet;

上述的nmax、nmin分别与核心层片层的折射率的最大值、最小值相同;The above n max and n min are respectively the same as the maximum value and minimum value of the refractive index of the core layer sheet;

具体地,例如m=2,则由公式(5)所限定的阻抗匹配层,靠近核心层的阻抗匹配层片层的折射率分布为:Specifically, for example, m=2, then the impedance matching layer defined by the formula (5), the refractive index distribution of the impedance matching layer near the core layer is:

nno 11 (( rr )) == nno minmin 11 22 ×× nno (( rr )) 11 22 ;;

靠近馈源的阻抗匹配层其折射率分布为:The refractive index distribution of the impedance matching layer close to the feed source is:

n2(r)=nminn 2 (r) = n min ;

当然,阻抗匹配层并不限于此,所述每一阻抗匹配层片层也可以具有单一的折射率,所述一个或多个阻抗匹配层片层的折射率满足以下公式:Of course, the impedance matching layer is not limited thereto, and each of the impedance matching layer sheets may also have a single refractive index, and the refractive index of the one or more impedance matching layer sheets satisfies the following formula:

nno (( ii )) == (( (( nno maxmax ++ nno minmin )) // 22 )) ii mm -- -- -- (( 66 )) ;;

其中,m表示阻抗匹配层的总层数,i表示阻抗匹配层片层的编号,其中,靠近核心层的阻抗匹配层片层的编号为m,由核心层向两侧方向,编号依次减小,两边最外侧的阻抗匹配层片层的编号为1,此处的n(r)表示核心层片层上半径为r处的折射率值。Among them, m represents the total number of layers of the impedance matching layer, and i represents the number of the impedance matching layer, wherein the number of the impedance matching layer near the core layer is m, and the number decreases in turn from the core layer to both sides. , the number of the outermost impedance matching layer on both sides is 1, where n(r) represents the refractive index value at the radius r on the core layer.

具体地,例如m=2,则由公式(6)所限定的阻抗匹配层,靠近核心层的阻抗匹配层片层的折射率分布为:Specifically, for example, m=2, then the impedance matching layer defined by formula (6), the refractive index distribution of the impedance matching layer near the core layer is:

n(2)=(nmax+nmin)/2;n(2)=(n max +n min )/2;

靠近馈源的阻抗匹配层其折射率分布为:The refractive index distribution of the impedance matching layer close to the feed source is:

nno (( 11 )) == (( (( nno maxmax ++ nno minmin )) // 22 )) 11 22 ;;

本实施例中,所述第二基材23包括片状的第二前基板231及第二后基板232,所述多个第二人造微结构夹设在第二前基板231与第二后基板232之间。所述阻抗匹配层片层的厚度为0.21-2.5mm,其中,第一前基板的厚度为0.1-1mm,第一后基板的厚度为0.1-1mm,多个第一人造微结构的厚度为0.01-0.5mm。优选地,所述阻抗匹配层片层的厚度为0.543mm,其中,第二前基板及第二后基板的厚度均为0.254mm,多个第二人造微结构的厚度为0.035mm。In this embodiment, the second substrate 23 includes a sheet-shaped second front substrate 231 and a second rear substrate 232, and the plurality of second artificial microstructures are sandwiched between the second front substrate 231 and the second rear substrate. Between 232. The thickness of the impedance matching layer is 0.21-2.5 mm, wherein the thickness of the first front substrate is 0.1-1 mm, the thickness of the first rear substrate is 0.1-1 mm, and the thickness of the plurality of first artificial microstructures is 0.01 mm. -0.5mm. Preferably, the thickness of the impedance matching layer is 0.543 mm, wherein the thickness of the second front substrate and the second rear substrate are both 0.254 mm, and the thickness of the plurality of second artificial microstructures is 0.035 mm.

本实施例中,所述第一人造微结构、第二人造微结构均为由铜线或银线构成的金属微结构,所述金属微结构通过蚀刻、电镀、钻刻、光刻、电子刻或离子刻的方法分别附着在第一基材、第二基材。优选地,所述第一人造微结构、第二人造微结构均为图5所示的平面雪花状的金属微结构通过拓扑形状演变得到的多个不同的拓扑形状的金属微结构。In this embodiment, the first artificial microstructure and the second artificial microstructure are metal microstructures composed of copper wires or silver wires, and the metal microstructures are formed by etching, electroplating, drilling, photolithography, electronic engraving, etc. Or the method of ion etching is respectively attached to the first substrate and the second substrate. Preferably, the first artificial microstructure and the second artificial microstructure are metal microstructures of multiple different topological shapes obtained by evolution of the planar snowflake-shaped metal microstructure shown in FIG. 5 through topological shape.

本实施例中,核心层片层可以通过如下方法得到,即在第一前基板与第一后基板的任意一个的表面上覆铜,再通过蚀刻的方法得到多个第一金属微结构(多个第一金属微结构的形状与排布事先通过计算机仿真获得),最后将第一前基板与第一后基板分别压合在一起,即得到本发明的核心层片层,压合的方法可以是直接热压,也可以是利用热熔胶连接,当然也可是其它机械式的连接,例如螺栓连接。In this embodiment, the core layer can be obtained by covering copper on the surface of any one of the first front substrate and the first rear substrate, and then obtaining a plurality of first metal microstructures (multiple first metal microstructures) by etching. The shape and arrangement of the first metal microstructure are obtained by computer simulation in advance), and finally the first front substrate and the first rear substrate are respectively pressed together to obtain the core layer of the present invention. The method of pressing can be It can be directly hot pressed, can also be connected by hot melt adhesive, and of course can also be connected by other mechanical methods, such as bolted connection.

同理,阻抗匹配层片层也可以利用相同的方法得到。然后分别将多个核心层片层压合一体,即形成了本发明的核心层;同样,将多个阻抗匹配层片层压合一体,即形成了本发明的阻抗匹配层;将核心层、阻抗匹配层压合一体即得到本发明的超材料平板。Similarly, the impedance matching layer can also be obtained by the same method. Then a plurality of core layers are laminated together to form the core layer of the present invention; similarly, a plurality of impedance matching layers are laminated to form the impedance matching layer of the present invention; the core layer, The impedance matching layers are laminated together to obtain the metamaterial flat plate of the present invention.

本实施例中,所述第一基材、第二基材由陶瓷材料、高分子材料、铁电材料、铁氧材料或铁磁材料等制得。高分子材料可选用的有F4B复合材料、FR-4复合材料等。In this embodiment, the first substrate and the second substrate are made of ceramic materials, polymer materials, ferroelectric materials, ferrite materials or ferromagnetic materials. Polymer materials can be selected from F4B composite materials, FR-4 composite materials, etc.

图5所示为平面雪花状的金属微结构的示意图,所述的雪花状的金属微结构具有相互垂直平分的第一金属线J1及第二金属线J2,所述第一金属线J1与第二金属线J2的长度相同,所述第一金属线J1两端连接有相同长度的两个第一金属分支F1,所述第一金属线J1两端连接在两个第一金属分支F1的中点上,所述第二金属线J2两端连接有相同长度的两个第二金属分支F2,所述第二金属线J2两端连接在两个第二金属分支F2的中点上,所述第一金属分支F1与第二金属分支F2的长度相等。5 is a schematic diagram of a plane snowflake-shaped metal microstructure. The snowflake-shaped metal microstructure has a first metal line J1 and a second metal line J2 that are perpendicular to each other. The lengths of the two metal wires J2 are the same, and the two ends of the first metal wire J1 are connected to two first metal branches F1 of the same length, and the two ends of the first metal wire J1 are connected to the center of the two first metal branches F1. In terms of point, the two ends of the second metal line J2 are connected to two second metal branches F2 of the same length, and the two ends of the second metal line J2 are connected to the midpoint of the two second metal branches F2. The lengths of the first metal branch F1 and the second metal branch F2 are equal.

图6是图5所示的平面雪花状的金属微结构的一种衍生结构。其在每个第一金属分支F1及每个第二金属分支F2的两端均连接有完全相同的第三金属分支F3,并且相应的第三金属分支F3的中点分别与第一金属分支F1及第二金属分支F2的端点相连。依此类推,本发明还可以衍生出其它形式的金属微结构。FIG. 6 is a derivative structure of the planar snowflake-like metal microstructure shown in FIG. 5 . Both ends of each first metal branch F1 and each second metal branch F2 are connected to identical third metal branches F3, and the midpoints of the corresponding third metal branches F3 are respectively connected to the first metal branch F1. and the terminal of the second metal branch F2 are connected. By analogy, the present invention can also derive other forms of metal microstructures.

图7是图5所示的平面雪花状的金属微结构的一种变形结构,此种结构的金属微结构,第一金属线J1与第二金属线J2不是直线,而是弯折线,第一金属线J1与第二金属线J2均设置有两个弯折部WZ,但是第一金属线J1与第二金属线J2仍然是垂直平分,通过设置弯折部的朝向与弯折部在第一金属线与第二金属线上的相对位置,使得图7所示的金属微结构绕垂直于第一金属线与第二金属线交点的轴线向任意方向旋转90度的图形都与原图重合。另外,还可以有其它变形,例如,第一金属线J1与第二金属线J2均设置多个弯折部WZ。FIG. 7 is a deformed structure of the plane snowflake-shaped metal microstructure shown in FIG. Both the metal wire J1 and the second metal wire J2 are provided with two bending parts WZ, but the first metal wire J1 and the second metal wire J2 are still perpendicularly bisected. The relative position of the metal line and the second metal line makes the pattern of the metal microstructure shown in FIG. 7 rotated 90 degrees in any direction around the axis perpendicular to the intersection of the first metal line and the second metal line coincide with the original figure. In addition, other deformations are also possible, for example, the first metal line J1 and the second metal line J2 are both provided with a plurality of bent portions WZ.

本实施例中,所述核心层片层11可以划分为阵列排布的多个如图2所示的超材料单元D,每个超材料单元D包括前基板单元U、后基板单元V及设置在基板单元U、后基板单元V之间的第一人造微结构12,通常超材料单元D的长宽高均不大于五分之一波长,优选为十分之一波长,因此,根据天线的工作频率可以确定超材料单元D的尺寸。图2为透视的画法,以表示第一人造微结构的超材料单元D中的位置,如图2所示,所述第一人造微结构夹于基板单元U、后基板单元V之间,其所在表面用SR表示。In this embodiment, the core layer sheet 11 can be divided into a plurality of metamaterial units D as shown in FIG. 2 arranged in an array, and each metamaterial unit D includes a front substrate unit U, a rear substrate unit V and a For the first artificial microstructure 12 between the substrate unit U and the rear substrate unit V, usually the length, width and height of the metamaterial unit D are not greater than one-fifth of the wavelength, preferably one-tenth of the wavelength. Therefore, according to the antenna The operating frequency can determine the size of the metamaterial unit D. Fig. 2 is a perspective drawing, to represent the position in the metamaterial unit D of the first artificial microstructure, as shown in Fig. 2, the first artificial microstructure is sandwiched between the substrate unit U and the rear substrate unit V, The surface on which it is located is represented by SR.

已知折射率

Figure BDA0000159140260000111
其中μ为相对磁导率,ε为相对介电常数,μ与ε合称为电磁参数。实验证明,电磁波通过折射率非均匀的介质材料时,会向折射率大的方向偏折。在相对磁导率一定的情况下(通常接近1),折射率只与介电常数有关,在第一基材选定的情况下,利用只对电场响应的第一人造微结构可以实现超材料单元折射率的任意值(在一定范围内),在该天线中心频率下,利用仿真软件,如CST、MATLAB、COMSOL等,通过仿真获得某一特定形状的人造微结构(如图5所示的平面雪花状的金属微结构)的介电常数随着拓扑形状的变化折射率变化的情况,即可列出一一对应的数据,即可设计出我们需要的特定折射率分布的核心层片层11,同理可以得到阻抗匹配层片层的折射率分布。known refractive index
Figure BDA0000159140260000111
Among them, μ is the relative magnetic permeability, ε is the relative permittivity, and μ and ε are collectively called electromagnetic parameters. Experiments have proved that when electromagnetic waves pass through a dielectric material with a non-uniform refractive index, they will be deflected toward the direction with a large refractive index. In the case of a certain relative magnetic permeability (usually close to 1), the refractive index is only related to the dielectric constant. In the case of the first substrate selected, metamaterials can be realized by using the first artificial microstructure that only responds to the electric field. Any value of the unit refractive index (within a certain range), under the center frequency of the antenna, use simulation software, such as CST, MATLAB, COMSOL, etc., to obtain an artificial microstructure of a specific shape through simulation (as shown in Figure 5 Planar snowflake-like metal microstructure) dielectric constant changes with the change of topological shape, the corresponding data can be listed, and the core layer of the specific refractive index distribution we need can be designed 11. Similarly, the refractive index distribution of the impedance matching layer can be obtained.

本实施例中,核心层片层的结构设计可通过计算机仿真(CST仿真)得到,具体如下:In this embodiment, the structural design of the core layer sheet can be obtained by computer simulation (CST simulation), as follows:

(1)确定第一金属微结构的附着基材(第一基材)。例如介电常数为2.25的介质基板,介质基板的材料可以是FR-4、F4b或PS。(1) Determine the attachment substrate (first substrate) of the first metal microstructure. For example, a dielectric substrate with a dielectric constant of 2.25, the material of the dielectric substrate can be FR-4, F4b or PS.

(2)确定超材料单元的尺寸。超材料单元的尺寸的尺寸由天线的中心频率得到,利用频率得到其波长,再取小于波长的五分之一的一个数值做为超材料单元D的长度CD与宽度KD。例如对应于11.95G的天线中心频率,所述超材料单元D为如图2所示的长CD与宽KD均为2.8mm、厚度HD为0.543mm的方形小板。(2) Determine the size of the metamaterial unit. The size of the metamaterial unit is obtained from the center frequency of the antenna, its wavelength is obtained by using the frequency, and a value less than one-fifth of the wavelength is taken as the length CD and width KD of the metamaterial unit D. For example, corresponding to the antenna center frequency of 11.95G, the metamaterial unit D is a small square plate with a length CD and a width KD of 2.8 mm and a thickness HD of 0.543 mm as shown in FIG. 2 .

(3)确定金属微结构的材料及拓扑结构。本发明中,金属微结构的材料为铜,金属微结构的拓扑结构为图5所示的平面雪花状的金属微结构,其线宽W各处一致;此处的拓扑结构,是指拓扑形状演变的基本形状。(3) Determine the material and topology of the metal microstructure. In the present invention, the material of the metal microstructure is copper, and the topological structure of the metal microstructure is a plane snowflake-like metal microstructure shown in Figure 5, and its line width W is consistent everywhere; the topological structure here refers to the topological shape Evolved basic shapes.

(4)确定金属微结构的拓扑形状参数。如图5所示,本发明中,平面雪花状的金属微结构的拓扑形状参数包括金属微结构的线宽W,第一金属线J1的长度a,第一金属分支F1的长度b。(4) Determine the topological shape parameters of the metal microstructure. As shown in FIG. 5 , in the present invention, the topological shape parameters of the planar snowflake-like metal microstructure include the line width W of the metal microstructure, the length a of the first metal line J1 , and the length b of the first metal branch F1 .

(5)确定金属微结构的拓扑形状的演变限制条件。本发明中,金属微结构的拓扑形状的演变限制条件有,金属微结构之间的最小间距WL(即如图5所示,金属微结构与超材料单元的长边或宽边的距离为WL/2),金属微结构的线宽W,超材料单元的尺寸;由于加工工艺限制,WL大于等于0.1mm,同样,线宽W也是要大于等于0.1mm。第一次仿真时,WL可以取0.1mm,W可以取0.3mm,超材料单元的尺寸为长与宽为2.8mm,厚度为0.543mm,此时金属微结构的拓扑形状参数只有a和b两个变量。金属微结构的拓扑形状通过如图7至图8所示的演变方式,对应于某一特定频率(例如11.95GHZ),可以得到一个连续的折射率变化范围。(5) Determine the evolution constraints of the topological shape of the metal microstructure. In the present invention, the evolution restriction condition of the topological shape of the metal microstructure has, the minimum spacing WL between metal microstructures (that is, as shown in Figure 5, the distance between the metal microstructure and the long side or wide side of the metamaterial unit is WL /2), the line width W of the metal microstructure, and the size of the metamaterial unit; due to the limitation of the processing technology, WL is greater than or equal to 0.1mm, and similarly, the line width W must also be greater than or equal to 0.1mm. In the first simulation, WL can be 0.1mm, W can be 0.3mm, the size of the metamaterial unit is 2.8mm in length and width, and the thickness is 0.543mm. At this time, the topological shape parameters of the metal microstructure are only a and b. variables. The topological shape of the metal microstructure corresponds to a specific frequency (for example, 11.95GHZ) through the evolution shown in Fig. 7 to Fig. 8, and a continuous range of refractive index variation can be obtained.

具体地,所述金属微结构的拓扑形状的演变包括两个阶段(拓扑形状演变的基本形状为图5所示的金属微结构):Specifically, the evolution of the topological shape of the metal microstructure includes two stages (the basic shape of the topological shape evolution is the metal microstructure shown in Figure 5):

第一阶段:根据演变限制条件,在b值保持不变的情况下,将a值从最小值变化到最大值,此演变过程中的金属微结构均为“十”字形(a取最小值时除外)。本实施例中,a的最小值即为0.3mm(线宽W),a的最大值为(CD-WL)。因此,在第一阶段中,金属微结构的拓扑形状的演变如图8所示,即从边长为W的正方形JX1,逐渐演变成最大的“十”字形拓扑形状JD1。在第一阶段中,随着金属微结构的拓扑形状的演变,与其对应的超材料单元的折射率连续增大(对应天线一特定频率)。The first stage: According to the evolution constraints, under the condition that the value of b remains unchanged, the value of a is changed from the minimum value to the maximum value. except). In this embodiment, the minimum value of a is 0.3 mm (line width W), and the maximum value of a is (CD-WL). Therefore, in the first stage, the evolution of the topological shape of the metal microstructure is shown in Figure 8, that is, it gradually evolves from a square JX1 with side length W to the largest topological shape JD1 of a "cross". In the first stage, as the topological shape of the metal microstructure evolves, the refractive index of the corresponding metamaterial unit increases continuously (corresponding to a specific frequency of the antenna).

第二阶段:根据演变限制条件,当a增加到最大值时,a保持不变;此时,将b从最小值连续增加到最大值,此演变过程中的金属微结构均为平面雪花状。本实施例中,b的最小值即为0.3mm,b的最大值为(CD-WL-2W)。因此,在第二阶段中,金属微结构的拓扑形状的演变如图9所示,即从最大的“十”字形拓扑形状JD1,逐渐演变成最大的平面雪花状的拓扑形状JD2,此处的最大的平面雪花状的拓扑形状JD2是指,第一金属分支J1与第二金属分支J2的长度b已经不能再伸长,否则第一金属分支与第二金属分支将发生相交。在第二阶段中,随着金属微结构的拓扑形状的演变,与其对应的超材料单元的折射率连续增大(对应天线一特定频率)。The second stage: According to the evolution constraints, when a increases to the maximum value, a remains unchanged; at this time, b is continuously increased from the minimum value to the maximum value, and the metal microstructure in this evolution process is planar snowflake shape. In this embodiment, the minimum value of b is 0.3 mm, and the maximum value of b is (CD-WL-2W). Therefore, in the second stage, the evolution of the topological shape of the metal microstructure is shown in Fig. 9, that is, from the largest "ten" topological shape JD1 to the largest planar snowflake-like topological shape JD2, where The largest planar snowflake topological shape JD2 means that the length b of the first metal branch J1 and the second metal branch J2 can no longer be extended, otherwise the first metal branch and the second metal branch will intersect. In the second stage, as the topological shape of the metal microstructure evolves, the refractive index of the corresponding metamaterial unit increases continuously (corresponding to a specific frequency of the antenna).

通过上述演变得到超材料单元的折射率变化范围如果包含了nmin至nmax的连续变化范围,则满足设计需要。如果上述演变得到超材料单元的折射率变化范围不满足设计需要,例如最大值太小或最小值过大,则变动WL与W,重新仿真,直到得到我们需要的折射率变化范围。Through the above evolution, if the refractive index variation range of the metamaterial unit includes the continuous variation range from n min to n max , it will meet the design requirements. If the range of refractive index variation of the metamaterial unit obtained from the above evolution does not meet the design requirements, for example, the maximum value is too small or the minimum value is too large, then change WL and W, and re-simulate until the desired range of refractive index variation is obtained.

根据公式(1)至(4),将仿真得到的一系列的超材料单元按照其对应的折射率排布以后(实际上就是不同拓扑形状的多个第一人造微结构在第一基材上的排布),即能得到本发明的核心层片层。According to formulas (1) to (4), after a series of metamaterial units obtained by simulation are arranged according to their corresponding refractive indices (actually, a plurality of first artificial microstructures with different topological shapes on the first substrate arrangement), that is, the core layer sheet of the present invention can be obtained.

同理,根据公式(5)-(6)可以得到本发明的阻抗匹配层片层。Similarly, the impedance matching layer of the present invention can be obtained according to formulas (5)-(6).

如图10所示,本发明的另一种实施例中,所述超材料平板100及超材料平板200不具有阻抗匹配层,其等效厚度D等于核心层厚度的两倍,其它的与上述的实施例相同。As shown in Figure 10, in another embodiment of the present invention, the metamaterial flat plate 100 and the metamaterial flat plate 200 do not have an impedance matching layer, and their equivalent thickness D is equal to twice the thickness of the core layer, and the others are the same as the above-mentioned The embodiment is the same.

上面结合附图对本发明的实施例进行了描述,但是本发明并不局限于上述的具体实施方式,上述的具体实施方式仅仅是示意性的,而不是限制性的,本领域的普通技术人员在本发明的启示下,在不脱离本发明宗旨和权利要求所保护的范围情况下,还可做出很多形式,这些均属于本发明的保护之内。Embodiments of the present invention have been described above in conjunction with the accompanying drawings, but the present invention is not limited to the above-mentioned specific implementations, and the above-mentioned specific implementations are only illustrative, rather than restrictive, and those of ordinary skill in the art will Under the enlightenment of the present invention, many forms can also be made without departing from the gist of the present invention and the protection scope of the claims, and these all belong to the protection of the present invention.

Claims (10)

1.一种动中通天线,其特征在于,所述动中通天线包括两个相同的方形超材料平板及设置在两个超材料平板之间的馈源,所述两个超材料平板的上边缘固定连接,馈源等效点在两个超材料平板上的投影与两个超材料平板的表面中心点重合,在伺服系统的控制下,所述馈源的开口始终正对更靠近通信卫星的那个超材料平板,所述两个超材料平板具有相同的折射率分布规律,每一超材料平板包括核心层,所述核心层包括一个核心层片层或多个相同的核心层片层,每一个核心层片层包括片状的第一基材以及设置在第一基材上的多个第一人造微结构,任一核心层片层的折射率分布满足如下公式:1. A communication antenna in motion, characterized in that, the communication antenna in motion comprises two identical square metamaterial flat panels and a feed source arranged between the two supermaterial flat panels, the two supermaterial flat panels The upper edge is fixedly connected, and the projection of the equivalent point of the feed source on the two metamaterial plates coincides with the center point of the surface of the two metamaterial plates. Under the control of the servo system, the opening of the feed source is always facing closer to the communication The metamaterial slab of the satellite, the two metamaterial slabs have the same refractive index distribution law, each metamaterial slab includes a core layer, and the core layer includes a core layer sheet or a plurality of identical core layer sheets , each core layer sheet includes a sheet-shaped first substrate and a plurality of first artificial microstructures disposed on the first substrate, and the refractive index distribution of any core layer sheet satisfies the following formula: nno (( rr )) == nno maxmax -- rr 22 ++ sthe s 22 -- VsegVseg DD. ;; Vseg=s+λ×NUMseg;Vseg=s+λ×NUMseg; NUMsegNUMseg == floorfloor {{ rr 22 ++ sthe s 22 -- sthe s λλ }} ;; DD. == λλ nno maxmax -- nno minmin ;; 其中,n(r)表示该核心层片层上半径为r处的折射率值,核心层片层的折射率分布圆心即为馈源等效点在该核心层片层表面的投影;Wherein, n(r) represents the refractive index value at the radius of r on the core layer sheet, and the center of the refractive index distribution circle of the core layer sheet is the projection of the equivalent point of the feed source on the surface of the core layer sheet; s为馈源等效点到超材料平板的垂直距离;s is the vertical distance from the feed equivalent point to the metamaterial plate; nmax表示核心层片层的折射率的最大值;n max represents the maximum value of the refractive index of the core layer sheet; nmin表示核心层片层的折射率的最小值;n min represents the minimum value of the refractive index of the core layer sheet; D为超材料平板的整体厚度;D is the overall thickness of the metamaterial slab; λ表示频率为天线中心频率的电磁波的波长;λ represents the wavelength of the electromagnetic wave whose frequency is the center frequency of the antenna; floor表示向下取整;floor means rounding down; 其中,两个超材料平板之间的夹角为θ,Among them, the angle between two metamaterial plates is θ, tgtg θθ 22 == 22 sthe s LL ;; L表示方形超材料平板构成θ夹角的两个边的长度。L represents the length of the two sides forming the included angle θ of the square metamaterial flat plate. 2.根据权利要求1所述的动中通天线,其特征在于,所述第一基材包括片状的第一前基板及第一后基板,所述多个第一人造微结构夹设在第一前基板与第一后基板之间,所述核心层片层的厚度为0.21-2.5mm,其中,第一前基板的厚度为0.1-1mm,第一后基板的厚度为0.1-1mm,多个第一人造微结构的厚度为0.01-0.5mm。2. The mobile communication antenna according to claim 1, wherein the first base material comprises a sheet-shaped first front substrate and a first rear substrate, and the plurality of first artificial microstructures are sandwiched between Between the first front substrate and the first rear substrate, the thickness of the core layer is 0.21-2.5mm, wherein the thickness of the first front substrate is 0.1-1mm, and the thickness of the first rear substrate is 0.1-1mm, The thickness of the plurality of first artificial microstructures is 0.01-0.5 mm. 3.根据权利要求2所述的动中通天线,其特征在于,所述核心层片层的厚度为0.543mm,其中,第一前基板及第一后基板的厚度均为0.254mm,多个第一人造微结构的厚度为0.035mm。3. The mobile communication antenna according to claim 2, characterized in that, the thickness of the core layer is 0.543mm, wherein the thickness of the first front substrate and the first rear substrate are both 0.254mm, a plurality of The thickness of the first artificial microstructure is 0.035mm. 4.根据权利要求1所述的动中通天线,其特征在于,每一超材料平板还包括设置在核心层两侧表面的阻抗匹配层,所述阻抗匹配层包括一个阻抗匹配层片层或多个厚度相同的阻抗匹配层片层,所述阻抗匹配层片层包括片状的第二基材以及设置在第二基材上的多个第二人造微结构,所述一个或多个阻抗匹配层片层的折射率分布满足如下公式:4. The communication-in-motion antenna according to claim 1, wherein each metamaterial slab also includes an impedance matching layer arranged on both sides of the core layer, and the impedance matching layer includes an impedance matching layer sheet or A plurality of impedance matching layers with the same thickness, the impedance matching layer includes a sheet-shaped second substrate and a plurality of second artificial microstructures arranged on the second substrate, the one or more impedance The refractive index distribution of the matching layer satisfies the following formula: nno ii (( rr )) == nno minmin ii mm ×× nno (( rr )) mm -- ii mm ;; 其中,ni(r)表示阻抗匹配层片层上半径为r处的折射率值,阻抗匹配层片层的折射率分布圆心即为馈源等效点在相应的阻抗匹配层片层外侧表面所在平面的投影;Among them, n i (r) represents the refractive index value at the radius r on the impedance matching layer, and the center of the refractive index distribution circle of the impedance matching layer is the equivalent point of the feed source on the outer surface of the corresponding impedance matching layer The projection of the plane on which it is located; 其中,i表示阻抗匹配层片层的编号,靠近核心层的阻抗匹配层片层的编号为1,两边最外侧的阻抗匹配层片层的编号为m,由核心层向两侧方向,编号依次减小;Among them, i represents the number of the impedance matching layer. The number of the impedance matching layer near the core layer is 1, and the number of the outermost impedance matching layer on both sides is m. From the core layer to the two sides, the numbers are sequential. decrease; 上述的nmax、nmin分别与核心层片层的折射率的最大值、最小值相同。The aforementioned n max and n min are respectively the same as the maximum and minimum values of the refractive index of the core layer sheet. 5.根据权利要求1所述的动中通天线,其特征在于,每一超材料平板还包括设置在核心层两侧表面的阻抗匹配层,所述阻抗匹配层包括一个阻抗匹配层片层或多个厚度相同的阻抗匹配层片层,所述阻抗匹配层片层包括片状的第二基材以及设置在第二基材上的多个第二人造微结构,所述每一阻抗匹配层片层具有单一的折射率,所述一个或多个阻抗匹配层片层的折射率满足以下公式:5. The communication-in-motion antenna according to claim 1, wherein each metamaterial slab also includes an impedance matching layer arranged on both surfaces of the core layer, and the impedance matching layer includes an impedance matching layer sheet or A plurality of impedance matching layers with the same thickness, the impedance matching layer includes a sheet-shaped second substrate and a plurality of second artificial microstructures arranged on the second substrate, each impedance matching layer The sheet has a single refractive index, and the refractive index of the one or more impedance matching layer sheets satisfies the following formula: nno (( ii )) == (( (( nno maxmax ++ nno minmin )) // 22 )) ii mm ;; 其中,m表示阻抗匹配层的总层数,i表示阻抗匹配层片层的编号,其中,靠近核心层的阻抗匹配层片层的编号为m,由核心层向两侧方向,编号依次减小,两边最外侧的阻抗匹配层片层的编号为1。Among them, m represents the total number of layers of the impedance matching layer, and i represents the number of the impedance matching layer, wherein the number of the impedance matching layer near the core layer is m, and the number decreases in turn from the core layer to both sides. , the number of the outermost impedance matching layer on both sides is 1. 6.根据权利要求3或4或5所述的动中通天线,其特征在于,所述第二基材包括片状的第二前基板及第二后基板,所述多个第二人造微结构夹设在第二前基板与第二后基板之间,所述阻抗匹配层片层的厚度为0.21-2.5mm,其中,第二前基板的厚度为0.1-1mm,第二后基板的厚度为0.1-1mm,多个第二人造微结构的厚度为0.01-0.5mm。6. The mobile communication antenna according to claim 3, 4 or 5, characterized in that, the second substrate comprises a sheet-shaped second front substrate and a second rear substrate, and the plurality of second artificial micro The structure is interposed between the second front substrate and the second rear substrate, and the thickness of the impedance matching layer is 0.21-2.5 mm, wherein the thickness of the second front substrate is 0.1-1 mm, and the thickness of the second rear substrate is is 0.1-1 mm, and the thickness of the plurality of second artificial microstructures is 0.01-0.5 mm. 7.根据权利要求1所述的动中通天线,其特征在于,所述第一人造微结构及第二人造微结构均为由铜线或银线构成的金属微结构,所述金属微结构通过蚀刻、电镀、钻刻、光刻、电子刻或离子刻的方法分别附着在第一基材及第二基材上。7. The mobile communication antenna according to claim 1, characterized in that, the first artificial microstructure and the second artificial microstructure are metal microstructures composed of copper wires or silver wires, and the metal microstructures They are respectively attached to the first substrate and the second substrate by means of etching, electroplating, drilling, photolithography, electron etching or ion etching. 8.根据权利要求7所述的动中通天线,其特征在于,所述金属微结构呈平面雪花状,所述金属微结构具有相互垂直平分的第一金属线及第二金属线,所述第一金属线与第二金属线的长度相同,所述第一金属线两端连接有相同长度的两个第一金属分支,所述第一金属线两端连接在两个第一金属分支的中点上,所述第二金属线两端连接有相同长度的两个第二金属分支,所述第二金属线两端连接在两个第二金属分支的中点上,所述第一金属分支与第二金属分支的长度相等。8. The mobile communication antenna according to claim 7, characterized in that, the metal microstructure is in the shape of a plane snowflake, and the metal microstructure has a first metal wire and a second metal wire that are perpendicular to each other and bisect each other. The length of the first metal wire is the same as that of the second metal wire, two first metal branches of the same length are connected to both ends of the first metal wire, and two ends of the first metal wire are connected to the two first metal branches. At the midpoint, the two ends of the second metal line are connected to two second metal branches of the same length, the two ends of the second metal line are connected to the midpoint of the two second metal branches, and the first metal The branch is equal in length to the second metal branch. 9.根据权利要求8所述的动中通天线,其特征在于,所述平面雪花状的金属微结构的每个第一金属分支及每个第二金属分支的两端还连接有完全相同的第三金属分支,相应的第三金属分支的中点分别与第一金属分支及第二金属分支的端点相连。9. The mobile communication antenna according to claim 8, characterized in that, the two ends of each first metal branch and each second metal branch of the planar snowflake-shaped metal microstructure are also connected with exactly the same For the third metal branch, the middle points of the corresponding third metal branch are respectively connected with the end points of the first metal branch and the second metal branch. 10.根据权利要求8所述的动中通天线,其特征在于,所述平面雪花状的金属微结构的第一金属线与第二金属线均设置有两个弯折部,所述平面雪花状的金属微结构绕第一金属线与第二金属线的交点在金属微结构所处平面内向任意方向旋转90度的图形都与原图重合。10. The mobile communication antenna according to claim 8, characterized in that, the first metal wire and the second metal wire of the planar snowflake-shaped metal microstructure are both provided with two bending parts, and the planar snowflake The shape of the metal microstructure rotated 90 degrees in any direction around the intersection of the first metal line and the second metal line in the plane where the metal microstructure is located coincides with the original figure.
CN201210132973.1A 2012-04-28 2012-04-28 Antenna for satellite communication in motion Active CN102709675B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210132973.1A CN102709675B (en) 2012-04-28 2012-04-28 Antenna for satellite communication in motion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210132973.1A CN102709675B (en) 2012-04-28 2012-04-28 Antenna for satellite communication in motion

Publications (2)

Publication Number Publication Date
CN102709675A true CN102709675A (en) 2012-10-03
CN102709675B CN102709675B (en) 2015-03-11

Family

ID=46902305

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210132973.1A Active CN102709675B (en) 2012-04-28 2012-04-28 Antenna for satellite communication in motion

Country Status (1)

Country Link
CN (1) CN102709675B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5657031A (en) * 1991-01-07 1997-08-12 Anderson; Fredrick C. Earth station antenna system
WO2005067615A2 (en) * 2004-01-07 2005-07-28 Motia Inc. Vehicle mounted satellite antenna system with in-motion tracking using beam forming
CN201285794Y (en) * 2008-10-17 2009-08-05 广州市易恒信息技术有限公司 A satellite antenna servo mechanism
CN101699659A (en) * 2009-11-04 2010-04-28 东南大学 Lens antenna
CN101867094A (en) * 2010-05-02 2010-10-20 兰州大学 A Focused Panel Antenna
CN201629405U (en) * 2010-03-02 2010-11-10 重庆航天新世纪卫星应用技术有限责任公司 In-motion satellite communication with eccentric azimuth spindle

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5657031A (en) * 1991-01-07 1997-08-12 Anderson; Fredrick C. Earth station antenna system
WO2005067615A2 (en) * 2004-01-07 2005-07-28 Motia Inc. Vehicle mounted satellite antenna system with in-motion tracking using beam forming
CN201285794Y (en) * 2008-10-17 2009-08-05 广州市易恒信息技术有限公司 A satellite antenna servo mechanism
CN101699659A (en) * 2009-11-04 2010-04-28 东南大学 Lens antenna
CN201629405U (en) * 2010-03-02 2010-11-10 重庆航天新世纪卫星应用技术有限责任公司 In-motion satellite communication with eccentric azimuth spindle
CN101867094A (en) * 2010-05-02 2010-10-20 兰州大学 A Focused Panel Antenna

Also Published As

Publication number Publication date
CN102709675B (en) 2015-03-11

Similar Documents

Publication Publication Date Title
CN102544717A (en) Lens antenna based on metamaterial
CN102723578B (en) Satellite antenna for satellite communication in motion
CN102480036A (en) Base station antenna
CN102480019A (en) Metamaterial antenna
CN102593606B (en) Metamaterial antenna of inclined reflect sheet and satellite television receiving system
CN102683818B (en) Antenna for satellite communication in motion
CN103094699B (en) Based on the lens antenna of Meta Materials
CN102683857B (en) Portable satellite antenna and satellite antenna receiving system
CN103367906B (en) Directional spreading antenna housing and directional antenna system
CN102680802B (en) Compact range generation device
CN103296458B (en) A kind of antenna for satellite communication in motion
CN102709675B (en) Antenna for satellite communication in motion
CN103367930B (en) Mobile communications antenna
CN103367927B (en) Logical satellite antenna during one is quiet
CN103367871B (en) A kind of antenna for satellite communication in motion
CN103367872B (en) A kind of antenna for satellite communication in motion
CN103296460B (en) Communication-on-the-move antenna
CN103367925B (en) Mobile communications antenna
CN103367929B (en) A kind of antenna for satellite communication in motion
CN103367873B (en) A kind of antenna for satellite communication in motion
CN102760950B (en) Portable satellite antenna and satellite antenna receiving system
CN102683811B (en) Metamaterial satellite antenna and satellite receiving system
CN102683813B (en) Satellite antenna for satellite communication in motion
CN103296457B (en) A kind of antenna for satellite communication in motion
CN103367928B (en) Logical satellite antenna during one is quiet

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
TR01 Transfer of patent right

Effective date of registration: 20210511

Address after: 2 / F, software building, No.9, Gaoxin Zhongyi Road, Nanshan District, Shenzhen City, Guangdong Province

Patentee after: KUANG-CHI INSTITUTE OF ADVANCED TECHNOLOGY

Address before: 18B, building a, CIC international business center, 1061 Xiangmei Road, Futian District, Shenzhen, Guangdong 518034

Patentee before: KUANG-CHI INNOVATIVE TECHNOLOGY Ltd.

TR01 Transfer of patent right