JPS6145605A - Antenna system of direction finding system - Google Patents
Antenna system of direction finding systemInfo
- Publication number
- JPS6145605A JPS6145605A JP16768884A JP16768884A JPS6145605A JP S6145605 A JPS6145605 A JP S6145605A JP 16768884 A JP16768884 A JP 16768884A JP 16768884 A JP16768884 A JP 16768884A JP S6145605 A JPS6145605 A JP S6145605A
- Authority
- JP
- Japan
- Prior art keywords
- antenna
- antennas
- direction finding
- circularly polarized
- polarized wave
- 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
Links
- 230000010287 polarization Effects 0.000 description 17
- 238000010586 diagram Methods 0.000 description 6
- 238000001514 detection method Methods 0.000 description 4
- 238000011088 calibration curve Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 101100234408 Danio rerio kif7 gene Proteins 0.000 description 1
- 101100221620 Drosophila melanogaster cos gene Proteins 0.000 description 1
- 101100398237 Xenopus tropicalis kif11 gene Proteins 0.000 description 1
- 101150118300 cos gene Proteins 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/24—Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction
- H01Q21/245—Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction provided with means for varying the polarisation
Landscapes
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
Description
【発明の詳細な説明】
〔発明の技術分野〕
この発明は、レーダ等の電波の到来方位を検出する方位
探知システムの空中線装置に関するものである。DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to an antenna device for a direction detection system that detects the arrival direction of radio waves such as radar.
方位探知システムの探知方式において、従来知られてい
る一方式として、振幅比較方式がある。As a detection method for a direction finding system, one conventionally known method is an amplitude comparison method.
第1図に振幅比較方式の方位探知システムの構成を示す
。第1図の装置は全方位360°を探知覆域とするもの
で、図において、1〜4は素子アンテナで、これら4つ
の素子アンテナ1〜4により、アンテナ部5が構成され
る。また6はスイッチ部で、2つの受信機7,8を4つ
の素子アンテナ1〜4のうちのいずれかの相隣り合う2
つの素子アンテナに接続する機能をもつ。9は2つの受
信機7.8の出力信号を比較し、方位を求める方位計算
部である。Figure 1 shows the configuration of an amplitude comparison type direction finding system. The device shown in FIG. 1 has a detection coverage area of 360° in all directions. In the figure, numerals 1 to 4 are element antennas, and these four element antennas 1 to 4 constitute an antenna section 5. Further, 6 is a switch section, which connects the two receivers 7 and 8 to any one of the four element antennas 1 to 4 adjacent to each other.
It has the function of connecting to two element antennas. Reference numeral 9 denotes an azimuth calculation unit that compares the output signals of the two receivers 7.8 and determines the azimuth.
次に動作について説明する。素子アンテナ1〜4は第2
図に示す如く、それぞれ1a〜4aの如き覆域をもつ。Next, the operation will be explained. Element antennas 1 to 4 are the second
As shown in the figure, each has a covering area such as 1a to 4a.
第2図において、θの方位から電波が到来したとき、素
子アンテナ1,2で受信される信号のレベルは、それぞ
れの素子アンテナのパターンによって決まるOA、OB
に比例している。この二つの信号OA、OBはスイッチ
部6によってそれぞれ受信機7.8に入力され、ここで
増幅、検波されて方位計算部9に入る。方位計算部9に
は、第3図に示す如く二つの信号の振幅比rと方位との
関係を記憶させであるので、方位針算部9はr−■/百
丁を求めて、記憶している振幅比rと方位角θとの関係
より電波の到来方位を求めることができる。例えば、二
つの素子アンテナ1.2のパターンが全く同じの場合は
、θ=45°のときにr−1である。In Fig. 2, when a radio wave arrives from the direction θ, the level of the signal received by element antennas 1 and 2 is determined by the pattern of each element antenna.
is proportional to. These two signals OA and OB are inputted by the switch section 6 to the receiver 7.8, where they are amplified and detected, and then input to the azimuth calculation section 9. Since the direction calculating section 9 is made to store the relationship between the amplitude ratio r of the two signals and the direction as shown in FIG. The direction of arrival of the radio wave can be determined from the relationship between the amplitude ratio r and the azimuth θ. For example, if the patterns of the two element antennas 1.2 are exactly the same, then r-1 when θ=45°.
一般に、素子アンテナのパターンは周波数特性をもって
おり、精度よく方位を探知する必要のある場合には、第
3図に示す振幅比rと方位角θの較正カーブを周波数の
ある一定範囲毎に記憶させておく必要がある。しかもこ
のとき、周波数情報を得る周波数分析回路が必要となる
。Generally, the pattern of an element antenna has frequency characteristics, and if it is necessary to detect the direction with high accuracy, a calibration curve of the amplitude ratio r and the direction angle θ shown in Fig. 3 should be memorized for each certain frequency range. It is necessary to keep it. Moreover, at this time, a frequency analysis circuit for obtaining frequency information is required.
従来の方位探知システムは以上のように構成されており
、任意の偏波面の電波を受けることができる円偏波アン
テナを使用しているが、一般的に偏波面に対する利得が
完全に一定なアンテナを得ることは非常に困難である。Conventional direction finding systems are configured as described above and use circularly polarized antennas that can receive radio waves of arbitrary polarization planes, but generally antennas whose gain is completely constant with respect to the polarization plane are used. It is very difficult to obtain.
第4図に素子アンテナ1.2のアンテナ・パターンの例
を示す。la。FIG. 4 shows an example of the antenna pattern of the element antenna 1.2. la.
2aは第2図と同じで、偏波特性のない理想的なパター
ンを示す。ここで一般的なアンテナパターンは例えば垂
直偏波に対してはlb、2bの如くなり、水平偏波に対
してはlc、2cの如くなる。2a is the same as FIG. 2 and shows an ideal pattern without polarization characteristics. Here, general antenna patterns are, for example, lb and 2b for vertically polarized waves, and lc and 2c for horizontally polarized waves.
この場合、電波到来方位θは振幅比r=oτ/百百によ
って与えられなければならないが、実際には垂直偏波が
来たときには振幅比rb=OAb10Bbとなり、水平
偏波が来たときには振幅比rc=OAc10Bcとなり
、これらの振幅比より得られる電波到来方位θb、θC
はrb<r<rCであるから第3図の較正カーブよりθ
b〉θ〉θCとなり、いずれのアンテナによっても正し
い方位は得られない。In this case, the radio wave arrival direction θ must be given by the amplitude ratio r=oτ/1000, but in reality, when a vertically polarized wave arrives, the amplitude ratio rb=OAb10Bb, and when a horizontally polarized wave arrives, the amplitude ratio rc=OAc10Bc, and radio wave arrival direction θb, θC obtained from these amplitude ratios
Since rb<r<rC, from the calibration curve in Fig. 3, θ
b>θ>θC, and the correct orientation cannot be obtained with any antenna.
この発明は、上記のような従来のものの欠点を除去する
ためになされたもので、同一構造の二つの円偏波アンテ
ナを開口面に垂直な軸に対して相互に直交するように配
置し、この二つのアンテナの出力を合成するように構成
したものを一つの素子アンテナとして使用することによ
り、偏波面の相違によって生ずる方位探知誤差を軽減す
ることができる方位探知システムの空中線装置を提供す
るものである。This invention was made in order to eliminate the drawbacks of the conventional antennas as described above. Two circularly polarized antennas having the same structure are arranged so as to be orthogonal to each other with respect to an axis perpendicular to the aperture surface. To provide an antenna device for an azimuth finding system that can reduce azimuth detection errors caused by differences in polarization planes by using an antenna configured to combine the outputs of these two antennas as one element antenna. It is.
以下、この発明の実施例を図について説明する。 Embodiments of the present invention will be described below with reference to the drawings.
第5図は代表的な円偏波アンテナであるスパイラルアン
テナの開口面を示す。第6図に第5図に示したスパイラ
ルアンテナの偏波特性を示し、第5図のアンテナ開口面
(x−y平面)に垂直な軸(2軸)回りの偏波面に対応
したアンテナの利得である。第6図において、偏波特性
のないどの偏波面の電波に対しても利得が一定な場合は
、円偏波アンテナの偏波特性はEの如く、円として表わ
される。しかるに一般に円偏波アンテナは、例えばEv
の如く垂直偏波に対しては利得が高(、水平偏波に対し
ては利得が低い楕円偏波特性をもっている。FIG. 5 shows the aperture of a spiral antenna, which is a typical circularly polarized antenna. Figure 6 shows the polarization characteristics of the spiral antenna shown in Figure 5. It's a gain. In FIG. 6, if the gain is constant for radio waves of any plane of polarization without polarization characteristics, the polarization characteristics of the circularly polarized antenna are expressed as a circle, as shown by E. However, in general, circularly polarized antennas, for example,
It has elliptical polarization characteristics, such as high gain for vertically polarized waves (low gain for horizontally polarized waves).
誉
巷こてこの発明の一実施例による方位探知システムの空
中線装置では、第5図に示すような同一構造の円偏波ア
ンテナ11.12二個を第7図に示す如く、それぞれ開
口面が2軸回りで90°異なるように配置し、この二つ
のアンテナ11.12の出力を加算器により合成するこ
とにより1つの素子アンテナ10を構成するようにして
いる。従ってアンテナ部5は複数個の素子アンテナ10
によって構成される。In an antenna device for a direction finding system according to an embodiment of the present invention, two circularly polarized antennas 11 and 12 having the same structure as shown in FIG. The antenna elements 11 and 12 are arranged to differ by 90 degrees around two axes, and the outputs of these two antennas 11 and 12 are combined by an adder to form one element antenna 10. Therefore, the antenna section 5 includes a plurality of element antennas 10.
Consisted of.
ここで素子アンテナ10の動作について説明する。第7
図のアンテナ11の偏波特性は第5図のアンテナと同じ
であり、第6図のEvの如く表わされるものとすると、
第7図のアンテナ12の偏波特性は、上述の如く、Ev
を2軸上で90°回転したものであるから第6図に重ね
て表わすとRhの如(なる。EV及びEhはそれぞれ楕
円として次式の如く表わすことができる。Here, the operation of the element antenna 10 will be explained. 7th
Assuming that the polarization characteristic of the antenna 11 in the figure is the same as that of the antenna in FIG. 5, and is expressed as Ev in FIG. 6,
As mentioned above, the polarization characteristics of the antenna 12 in FIG. 7 are Ev
is rotated by 90 degrees on two axes, so when it is superimposed on FIG. 6, it looks like Rh. EV and Eh can each be expressed as ellipses as shown in the following equation.
今、任意の偏波面φの電波が到来したとき、アンテナ1
1及び12で受ける信号のレベルは第6図に示す如(、
ψ方向を示す直線と、Ev、及びRhの交点として表わ
され、それぞれOP、OQに比例した値として示される
。lv、Ehはそれぞれ上式の如き楕円であるからOP
、OQは次の如く表すことができる。Now, when a radio wave with an arbitrary polarization plane φ arrives, antenna 1
The levels of the signals received at nodes 1 and 12 are as shown in FIG.
It is expressed as the intersection of Ev and Rh with a straight line indicating the ψ direction, and is expressed as a value proportional to OP and OQ, respectively. Since lv and Eh are ellipses as shown in the above formula, OP
, OQ can be expressed as follows.
OF2 = (ncos φ) 2 + (ms
in φ)2−σQ2 = (mcos φ) 2
+ (nsin φ)2従ってアンテナ11とアン
テナ12で受ける信号の電力を加算して得られる信号は
万下2+百百2− (n2 +m2 )・ (cos2
φ+sin 2φ)
1”n2+ff12
となり、φに無関係な一定値となる。このことから偏波
特性のある二つの同じアンテナを第7図の如く配置しそ
れぞれの信号を加算して得られる信号は等価的な偏波特
性がなくなることが判る。OF2 = (n cos φ) 2 + (ms
in φ)2−σQ2 = (mcos φ) 2
+ (nsin φ)2 Therefore, the signal obtained by adding the powers of the signals received by antennas 11 and 12 is 2 + 100 2 - (n2 + m2) (cos2)
φ+sin 2φ) 1"n2+ff12, which is a constant value independent of φ. From this, the signals obtained by arranging two identical antennas with polarization characteristics as shown in Figure 7 and adding their respective signals are equivalent. It can be seen that the polarization characteristics disappear.
このように、本実施例の構成によれば、素子アンテナを
、同一構造の二つの円偏波アンテナを2軸に関して90
°交叉するように配置して組合わせ、そのアンテナ出力
を加算器で合成するように構成したので、二つの円偏波
アンテナの偏波特性が互いに打消され、方位探知システ
ムにおいて偏波面の相違に基く方位の探知誤差が軽減さ
れる効果がある。As described above, according to the configuration of this embodiment, the element antenna is configured such that two circularly polarized antennas of the same structure are connected at 90° with respect to the two axes.
° Since the configuration is such that they are arranged and combined so that they intersect, and their antenna outputs are combined using an adder, the polarization characteristics of the two circularly polarized antennas cancel each other out, and the polarization plane differs in the direction finding system. This has the effect of reducing the error in detecting direction based on .
なお、上記実施例では円偏波アンテナとしてスパイラル
アンテナを用いたものを示したが、円偏波アンテナであ
れば同じ効果が得られることはいうまでもない。In the above embodiment, a spiral antenna is used as the circularly polarized antenna, but it goes without saying that the same effect can be obtained using a circularly polarized antenna.
また、上記実施例では方位探知システムの空中線装置と
して、従来方式の素子アンテナを本発明による素子アン
テナに置き換えるようにしたものについて説明したが、
方位探知システムの空中線装置は第1図の空中線部5に
示す全方位を4つの素子アンテナでカバーする方式の他
、6つの素子アンテナを使うもの、あるいはさらに多く
の素子アンテナを使うもの等があるが、いずれの場合に
も本発明による素子アンテナを用いることにより、同じ
効果が得られることはいうまでもない。Furthermore, in the above embodiment, an antenna device for a direction finding system was described in which a conventional element antenna was replaced with an element antenna according to the present invention.
Antenna devices for direction finding systems include those that use four element antennas to cover all directions as shown in the antenna section 5 in Figure 1, as well as those that use six element antennas, or those that use even more element antennas. However, it goes without saying that in any case, the same effect can be obtained by using the element antenna according to the present invention.
以上のように、この発明に係る方位探知システムの空中
線装置によれば、同一構造の二つの円偏波アンテナを開
口面に垂直な軸に対して相互に直交するように配置しこ
の二つのアンテナの出力を合成するように構成すること
により、偏波特性がない素子アンテナが得られ、これを
用いて空中線装置を構成するようにしたので、方位探知
精度の高いシステムを提供することが可能となる効果が
ある。As described above, according to the antenna device of the direction finding system according to the present invention, two circularly polarized antennas having the same structure are arranged so as to be orthogonal to each other with respect to an axis perpendicular to the aperture plane. By configuring the antenna to combine the outputs of the antenna, an element antenna with no polarization characteristics is obtained, and this is used to configure the antenna device, making it possible to provide a system with high azimuth finding accuracy. This has the effect of
第1図は方位探知システムの構成を示す図、第2図、第
3図は方位探知システムの動作原理を示す図、第4図は
従来の方位探知システムの空中線装置の欠点を説明する
図、第5図は第1図の空中線装置を構成する従来の素子
アンテナの例を示す図、第6図は従来のものと本発明の
一実施例による方位探知システムの空中線装置の素子ア
ンテナの動作を説明する図、第7図は本実施例装置の素
子アンテナの構成を示す図である。
図において、1〜4は素子アンテナ、5は空中線部、1
0は素子アンテナ、11.12は素子アンテナlOを構
成する円偏波アンテナである。FIG. 1 is a diagram showing the configuration of the direction finding system, FIGS. 2 and 3 are diagrams showing the operating principle of the direction finding system, and FIG. 4 is a diagram explaining the drawbacks of the antenna device of the conventional direction finding system. FIG. 5 is a diagram showing an example of a conventional element antenna constituting the antenna device shown in FIG. The explanatory diagram, FIG. 7, is a diagram showing the configuration of the element antenna of the device of this embodiment. In the figure, 1 to 4 are element antennas, 5 is an antenna section, 1
0 is an element antenna, and 11.12 is a circularly polarized antenna forming the element antenna IO.
Claims (1)
いて、その素子アンテナとして、開口面に垂直な軸に対
して相互に直交するように配置された同一構造の二つの
円偏波アンテナと、該両円偏波アンテナの出力を合成す
る加算器とからなる素子アンテナを用いたことを特徴と
する方位探知システムの空中線装置。(1) In an antenna device for an amplitude comparison type direction finding system, its element antennas include two circularly polarized antennas of the same structure arranged so as to be orthogonal to each other with respect to an axis perpendicular to the aperture plane, and An antenna device for a direction finding system characterized by using an element antenna consisting of an adder that combines the outputs of circularly polarized antennas.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP16768884A JPS6145605A (en) | 1984-08-09 | 1984-08-09 | Antenna system of direction finding system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP16768884A JPS6145605A (en) | 1984-08-09 | 1984-08-09 | Antenna system of direction finding system |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6145605A true JPS6145605A (en) | 1986-03-05 |
JPH0523521B2 JPH0523521B2 (en) | 1993-04-05 |
Family
ID=15854384
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP16768884A Granted JPS6145605A (en) | 1984-08-09 | 1984-08-09 | Antenna system of direction finding system |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6145605A (en) |
-
1984
- 1984-08-09 JP JP16768884A patent/JPS6145605A/en active Granted
Also Published As
Publication number | Publication date |
---|---|
JPH0523521B2 (en) | 1993-04-05 |
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