JPH04157383A - Measuring apparatus of azimuth - Google Patents
Measuring apparatus of azimuthInfo
- Publication number
- JPH04157383A JPH04157383A JP28121790A JP28121790A JPH04157383A JP H04157383 A JPH04157383 A JP H04157383A JP 28121790 A JP28121790 A JP 28121790A JP 28121790 A JP28121790 A JP 28121790A JP H04157383 A JPH04157383 A JP H04157383A
- Authority
- JP
- Japan
- Prior art keywords
- difference
- azimuth
- phase
- antenna element
- elements
- 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.)
- Pending
Links
- 238000005259 measurement Methods 0.000 abstract description 7
- 238000010586 diagram Methods 0.000 description 7
- 238000000605 extraction Methods 0.000 description 3
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000002253 acid Substances 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
Landscapes
- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は複数個の空中線素子を円周上に等間隔に配置し
、これらの空中線を順次切換え走査して到来電波の方位
を計測す′る方位測定装置に関する。[Detailed Description of the Invention] [Field of Industrial Application] The present invention measures the direction of incoming radio waves by arranging a plurality of antenna elements at equal intervals on the circumference and scanning these antennas by sequentially switching them. This invention relates to a direction measuring device.
従来の方位測定装置は、第5図に示すように、複数の空
中線素子1を円周上に等間隔に配置した円形アレー空中
線と、無指向性の空中線素子2と、方位測定装置3とで
構成されている。As shown in FIG. 5, the conventional azimuth measuring device includes a circular array antenna in which a plurality of antenna elements 1 are arranged at equal intervals on the circumference, a non-directional antenna element 2, and a azimuth measuring device 3. It is configured.
方位測定装置3は、基準信号発生器36により前記空中
線素子1を電気的に順次切り換えて走査を行い、得られ
た信号を周波数変換器31でIF信号に周波数変換し、
サイドバンドキャンセラ34を通した上で方位計測器3
5に入力させる。このとき、空中線素子1の切り換え走
査によって第6図(a)のように受信位相が正弦波状に
変化される受信信号S1が得られ、これを位相検波する
ことで同図に破線で示す正弦波状の検波信号S、1を得
ることができる。そして、この信号と、第6図(b)の
ような前記基準信号発生器36の基準信号S、とを比較
することで、到来信号の方位θを計測することが可能と
なる。The direction measuring device 3 performs scanning by sequentially electrically switching the antenna element 1 using a reference signal generator 36, and converts the frequency of the obtained signal into an IF signal using a frequency converter 31.
After passing through the sideband canceller 34, the direction measuring device 3
5. At this time, by switching and scanning the antenna element 1, a reception signal S1 whose reception phase changes in a sinusoidal manner as shown in FIG. A detected signal S,1 can be obtained. By comparing this signal with the reference signal S of the reference signal generator 36 as shown in FIG. 6(b), it becomes possible to measure the direction θ of the incoming signal.
なお、無指向性の空中線素子2では常時受信を行ってお
り、この受信信号を第5図のように、局発33を共通利
用した周波数変換器32で周波数変換し、そのIF倍信
号空中線素子lからのIF倍信号共にサイドバンドキャ
ンセラ34に入力することで方位計測に不要な信号を除
去している。In addition, the omnidirectional antenna element 2 is constantly receiving signals, and as shown in FIG. By inputting both the IF multiplied signal from 1 to the sideband canceller 34, unnecessary signals for direction measurement are removed.
つまり、空中線素子1は受信切換えられる結果、この切
換周期(周波数)と同じ成分の信号を含むことになり、
元の受信信号にこの近傍の変調成分(特にFM酸成分が
入っていると、前記信号と干渉し、方位測定結果に誤差
が生じてくる。このため、方位信号を含む受信信号と、
方位信号を含まない受信信号とで差分をとることにより
、サイドバンドキャンセラ34において方位測定に必要
な成分のみを抽出している。In other words, as a result of receiving switching, the antenna element 1 contains a signal with the same component as this switching period (frequency),
If the original received signal contains a modulation component (especially an FM acid component) in the vicinity, it will interfere with the signal and cause an error in the direction measurement result.For this reason, the received signal including the direction signal,
By taking the difference between the received signal and the received signal that does not include the azimuth signal, the sideband canceller 34 extracts only the components necessary for azimuth measurement.
この従来の方位測定装置では、円周上に等間隔に配設し
た空中線素子1と、無指向性の空中線素子20両空中線
で受信する信号を処理することにより、電波の到来方向
を計測している。このため、平面的な方位角は計測可能
であるが、電波の入射 ′角(エレベーションアング
ル)を測定することができないという問題がある。This conventional direction measuring device measures the direction of arrival of radio waves by processing signals received by both antennas: antenna elements 1 and omnidirectional antenna elements 20 arranged at equal intervals on the circumference. There is. For this reason, although it is possible to measure the plane azimuth angle, there is a problem in that the angle of incidence (elevation angle) of the radio waves cannot be measured.
本発明の目的は、入射角の測定を可能とした方位測定装
置を提供することにある。An object of the present invention is to provide an azimuth measuring device that can measure the angle of incidence.
〔課題を解決するための手段]
本発明の方位測定装置は、−の空中線素子で受信する到
来信号の位相と、この空中線素子と上下方向に異なる位
置に配置した他の空中線素子で受信する到来信号位相を
比較する手段を有し、この比較手段により到来電波の方
位と到来入射角を計測するように構成している。[Means for Solving the Problems] The direction measuring device of the present invention is capable of determining the phase of an incoming signal received by a negative antenna element, and the phase of an incoming signal received by another antenna element disposed at a position vertically different from this antenna element. It has means for comparing signal phases, and is configured to measure the azimuth and arrival angle of the arriving radio waves using this comparing means.
比較手段は、両空中線素子の位相差の差分をとる差分回
路と、この差分が最小になるように一方の位相を制御す
る移相器とで構成される。The comparison means is comprised of a difference circuit that takes the difference in phase difference between both antenna elements, and a phase shifter that controls one phase so that this difference is minimized.
本発明によれば、上下方向に配設した各空中線素子の位
相差を利用することで、方位計測と同時に入射角の計測
が可能となる。According to the present invention, by utilizing the phase difference between the antenna elements disposed in the vertical direction, it is possible to measure the angle of incidence simultaneously with the measurement of the azimuth.
次に、本発明を図面を参照して説明する。 Next, the present invention will be explained with reference to the drawings.
第1図は本発明の方位−窓装置の全体構成図であり、そ
のアンテナ部分は第2図に示すように、円周上に等間隔
に配置した複数の空中線素子1と、これら空中線素子1
の円周中心位置に設けて各空中線素子1よりも上下方向
に異なる位置に配置した無指向性の空中線素子2とで構
成されている。FIG. 1 is an overall configuration diagram of the azimuth-window device of the present invention, and its antenna portion, as shown in FIG. 2, includes a plurality of antenna elements 1 arranged at equal intervals on the circumference, and these antenna elements
, and a non-directional antenna element 2 disposed at a position vertically different from each antenna element 1.
この構成は従来のアンテナ構成がそのまま利用できる。With this configuration, the conventional antenna configuration can be used as is.
そして、前記空中線素子1と空中線素子2はそれぞれ従
来と同様に構成された方位測定装置3と、入射角抽出部
4に接続されている。この入射角抽出部4は、空中線素
子1からの信号を移相する移相器4工と、空中線素子2
との位相差をとる差分回路42を備え、この位相差に基
づいて処理器5で入射角を計測するように構成されてい
る。The antenna element 1 and the antenna element 2 are connected to an azimuth measuring device 3 and an incident angle extracting section 4, respectively, which are constructed in the same manner as in the prior art. The angle of incidence extraction unit 4 includes a phase shifter 4 that shifts the phase of the signal from the antenna element 1, and an antenna element 2.
The processor 5 is configured to include a difference circuit 42 that calculates the phase difference between the two and the processor 5 to measure the angle of incidence based on this phase difference.
この構成によれば、方位測定装置3では空中線素子1と
無指向性の空中線素子2とを利用して従来と同様に方位
角を計測するこができる。According to this configuration, the azimuth measuring device 3 can measure the azimuth using the antenna element 1 and the non-directional antenna element 2 in the same manner as in the past.
一方、入射角抽出部4では、空中線素子lと空中線素子
3との信号により入射角ψを計測することができる。第
3図はその原理を示す図であり、この図は説明の便宜上
、空中線素子1,2を上。On the other hand, the angle of incidence extraction section 4 can measure the angle of incidence ψ based on the signals from the antenna elements 1 and 3. FIG. 3 is a diagram showing the principle, and for convenience of explanation, the antenna elements 1 and 2 are shown at the top.
下に直線的に配置し、上方から電波を受信した状態を示
している。この場合の入射角φ、とすると、空中線素子
1と空中線素子2で受信する時の位相差Δφは、
となる。It is arranged in a straight line below, and shows the state in which radio waves are received from above. If the angle of incidence in this case is φ, then the phase difference Δφ when receiving by antenna element 1 and antenna element 2 is as follows.
なお、d、は空中線1と2の直線上での上下間距離であ
る。Note that d is the vertical distance between the antennas 1 and 2 on a straight line.
これから、Δψを求めれば入射角ψ、を計測することか
できる。From this, if Δψ is found, the angle of incidence ψ can be measured.
すなわち、第1図の構成においては、両空中線素子1.
2からの信号を入射角抽出部4に入力し、その差分回路
42で両信号の位相の差分をとり、その差分が最小にな
るように移相器41を調整すれば、その時の移相器の変
位量がΔψに相当する。That is, in the configuration of FIG. 1, both antenna elements 1.
2 is input to the incident angle extractor 4, the difference circuit 42 calculates the phase difference between the two signals, and the phase shifter 41 is adjusted so that the difference is minimized. The amount of displacement corresponds to Δψ.
なお、前記実施例では、空中線素子1と空中線素子2と
が直線上で上下に位置されていた例を示しているが、実
際には空中線素子1と空中線素子2が直線上の上下関係
になっていない。この場合も原理的には前述と同じ手法
で入射角の計測を行うことができる。つまり、第4図に
示すように、空中線素子1と空中線素子2の受信信号位
相差ψは、
から求めることができる。Although the above embodiment shows an example in which the antenna element 1 and the antenna element 2 are located vertically on a straight line, in reality, the antenna element 1 and the antenna element 2 are located vertically on a straight line. Not yet. In this case as well, the angle of incidence can be measured in principle using the same method as described above. That is, as shown in FIG. 4, the received signal phase difference ψ between the antenna element 1 and the antenna element 2 can be determined from the following equation.
なお、は両空中線素子1.2の水平距離である。Note that is the horizontal distance between both antenna elements 1.2.
これから前述の原理で説明したような方法でψを抽出す
ることにより、入射角ψ2を計測することができる。From this, the incident angle ψ2 can be measured by extracting ψ using the method explained in the above-mentioned principle.
以上説明したように本発明は、上下方向に異なる位置に
配設したーの空中線素子と他の空中線素子の各信号の位
相を比較することで、方位計測と同時に入射角を計測で
きる効果がある。As explained above, the present invention has the effect of being able to measure the angle of incidence at the same time as the azimuth measurement by comparing the phases of the signals of the antenna element and the other antenna elements arranged at different positions in the vertical direction. .
また、比較手段では、両空中線素子の信号位相の差分が
最小になるように一方の位相を移相器で調整することで
、その際の移相器の変位量が位相差として得ることがで
きる。In addition, in the comparison means, by adjusting one phase using a phase shifter so that the difference between the signal phases of both antenna elements is minimized, the amount of displacement of the phase shifter at that time can be obtained as a phase difference. .
第1図は本発明の方位計測装置の一実施例のブロック図
、第2図はアンテナ部分の構成図、第3図は入射角を計
測する原理を説明するための図、第4図は異なる空中線
配置の場合の入射角を計測する原理を説明するための図
、第5図は従来の方位測定装置のブロック図、第6図(
a)および(b)はそれぞれ方位を計測する際の信号波
形図である。
1.2・・・空中線素子、3・・・方位測定装置、4・
・・入射角抽出部、5・・・処理器、31.32・・・
周波数変換器、33・・・局発、34・・・サイドバン
ドキャンセラ、35・・・方位計測器、36・・・基準
信号発生器、41・・・移相器、42・・・差分回路。
第1図
第3図 第4図
σ2
第6図Fig. 1 is a block diagram of one embodiment of the direction measuring device of the present invention, Fig. 2 is a configuration diagram of the antenna part, Fig. 3 is a diagram for explaining the principle of measuring the angle of incidence, and Fig. 4 is different. Figure 5 is a block diagram of a conventional direction measuring device, and Figure 6 (
(a) and (b) are signal waveform diagrams when measuring the azimuth, respectively. 1.2...Antenna element, 3...Direction measuring device, 4.
...Incidence angle extraction unit, 5...Processor, 31.32...
Frequency converter, 33... Local oscillator, 34... Sideband canceller, 35... Direction measuring device, 36... Reference signal generator, 41... Phase shifter, 42... Differential circuit . Figure 1 Figure 3 Figure 4 σ2 Figure 6
Claims (1)
の空中線素子を電気的に順次切り換えることにより得ら
れる隣接空中線素子間位相に基づいて到来電波の方位を
測定する方位測定装置において、前記空中線素子で受信
する到来信号の位相と、前記空中線素子と上下方向に異
なる位置に配置した他の空中線素子で受信する到来信号
位相を比較する手段を有し、この比較手段により到来電
波の方位と到来入射角を計測することを特徴とする方位
測定装置。 2、比較手段は、両空中線素子の位相差の差分をとる差
分回路と、この差分が最小になるように一方の位相を制
御する移相器とで構成されてなる特許請求の範囲第1項
記載の方位測定装置。[Claims] 1. The direction of the incoming radio wave is determined based on the phase between adjacent antenna elements obtained by arranging a plurality of antenna elements at equal intervals on the circumference and electrically switching the antenna elements sequentially. The azimuth measuring device for measuring includes means for comparing the phase of an incoming signal received by the antenna element with the phase of an incoming signal received by another antenna element disposed at a position different from the antenna element in the vertical direction, An azimuth measuring device characterized by measuring the azimuth and the angle of incidence of incoming radio waves using comparison means. 2. Claim 1, wherein the comparison means is comprised of a difference circuit that takes the difference in phase difference between both antenna elements, and a phase shifter that controls the phase of one of the antennas so that this difference is minimized. The orientation measuring device described.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP28121790A JPH04157383A (en) | 1990-10-19 | 1990-10-19 | Measuring apparatus of azimuth |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP28121790A JPH04157383A (en) | 1990-10-19 | 1990-10-19 | Measuring apparatus of azimuth |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH04157383A true JPH04157383A (en) | 1992-05-29 |
Family
ID=17635999
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP28121790A Pending JPH04157383A (en) | 1990-10-19 | 1990-10-19 | Measuring apparatus of azimuth |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH04157383A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2008249354A (en) * | 2007-03-29 | 2008-10-16 | Nec Corp | Azimuth measuring device |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60143793A (en) * | 1983-12-29 | 1985-07-30 | Koden Electronics Co Ltd | Radio direction finder |
-
1990
- 1990-10-19 JP JP28121790A patent/JPH04157383A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60143793A (en) * | 1983-12-29 | 1985-07-30 | Koden Electronics Co Ltd | Radio direction finder |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2008249354A (en) * | 2007-03-29 | 2008-10-16 | Nec Corp | Azimuth measuring device |
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