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JPS5926909B2 - Interference wave direction separation device for direction finder - Google Patents
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JPS5926909B2 - Interference wave direction separation device for direction finder - Google Patents

Interference wave direction separation device for direction finder

Info

Publication number
JPS5926909B2
JPS5926909B2 JP10441180A JP10441180A JPS5926909B2 JP S5926909 B2 JPS5926909 B2 JP S5926909B2 JP 10441180 A JP10441180 A JP 10441180A JP 10441180 A JP10441180 A JP 10441180A JP S5926909 B2 JPS5926909 B2 JP S5926909B2
Authority
JP
Japan
Prior art keywords
output
separation device
interference wave
detecting
phase
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP10441180A
Other languages
Japanese (ja)
Other versions
JPS5729967A (en
Inventor
憲三 森
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.)
Taiyo Musen Co Ltd
Original Assignee
Taiyo Musen Co 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 Taiyo Musen Co Ltd filed Critical Taiyo Musen Co Ltd
Priority to JP10441180A priority Critical patent/JPS5926909B2/en
Publication of JPS5729967A publication Critical patent/JPS5729967A/en
Publication of JPS5926909B2 publication Critical patent/JPS5926909B2/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S3/00Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/02Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
    • G01S3/14Systems for determining direction or deviation from predetermined direction
    • G01S3/58Rotating or oscillating beam systems using continuous analysis of received signal for determining direction in the plane of rotation or oscillation or for determining deviation from a predetermined direction in such a plane
    • G01S3/60Broad-beam systems producing in the receiver a substantially sinusoidal envelope signal of the carrier wave of the beam, the phase angle of which is dependent upon the angle between the direction of the transmitter from the receiver and a reference direction from the receiver, e.g. cardioid system

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Description

【発明の詳細な説明】 指向性のある空中線自体またはその出力を加えられるゴ
ニオメータを機械的に回転するか、あるいは空中線の出
力を低周波信号で平衡変調する等の純電気的方法でその
指向性を実質的に回転させることにより電波の到来方向
を知ることができる。
DETAILED DESCRIPTION OF THE INVENTION The directivity of the antenna can be determined by mechanically rotating the directional antenna itself or a goniometer to which its output is applied, or by purely electrical methods such as balanced modulation of the antenna's output with a low frequency signal. The direction of arrival of radio waves can be determined by substantially rotating the .

このような方向探知機において、もし混信波があると従
来はその合成出力に対応する方向が指示されたから大き
な誤観測を生ずるおそれがあった。
In such a direction finder, if there was interference waves, conventionally the direction corresponding to the combined output was indicated, which could lead to large erroneous observations.

従って本発明は2つの混信波が受信された場合に、その
各々の電波の到来方向を分別して別個に測定することが
できるようにしたものである。
Therefore, in the present invention, when two interference waves are received, the direction of arrival of each radio wave can be separated and measured separately.

第1図は本発明の一実施例で指向性のある2つのループ
アンテナ1,2をその指向性が直交するように配置して
、出力を平衡変調器3,4に加えである。
FIG. 1 shows an embodiment of the present invention in which two directional loop antennas 1 and 2 are arranged so that their directivities are orthogonal to each other, and their outputs are applied to balanced modulators 3 and 4.

また低周波発振器5から互に90度の位相差を有する2
つの出力を取り出して、その各々を上記変調器3および
4に加えて、前記空中線出力を平衡変調し、合成器6に
加えである。
In addition, from the low frequency oscillator 5, two waves having a phase difference of 90 degrees are generated.
The antenna output is balanced modulated by taking two outputs and applying each of them to the modulators 3 and 4 above, and adding them to the combiner 6.

この合成器6には更にスイッチ7を介して、無指向性空
中線8の出力を移相器9で90度位相させた出力を加え
である。
To this combiner 6 is further added via a switch 7 an output obtained by shifting the output of the omnidirectional antenna 8 by 90 degrees from a phase shifter 9.

上記合成器6の出力を受信部10に加えて、増幅並びに
周波数変換等を行い、その出力を検波器11に加えであ
る。
The output of the synthesizer 6 is applied to a receiving section 10 for amplification, frequency conversion, etc., and the output is applied to a detector 11.

また検波器11の出力を帯域除去済波器12に加えてこ
れに含まれる低周波分を除去し、同調増幅器13を介し
てその出力を検波器14に加えである。
Further, the output of the wave detector 11 is applied to a band-removed wave detector 12 to remove the low frequency components contained therein, and the output is applied to a wave detector 14 via a tuned amplifier 13.

切換スイッチ15によって上記検波器11または14の
出力を、発振器5から得られる基準位相の低周波信号と
共にブラウン管駆動回路16に加え、該回路の出力をブ
ラウン管17の偏向板および電子流制御格子に加えであ
る。
The changeover switch 15 applies the output of the detector 11 or 14 to the cathode ray tube drive circuit 16 together with the low frequency signal of the reference phase obtained from the oscillator 5, and the output of the circuit is applied to the deflection plate of the cathode ray tube 17 and the electron flow control grid. It is.

上述の装置において、混信波が存在しない場合は図のよ
うに検波器11の出力を駆動回路16に加えると共にま
ずスイッチ7を開放して観測を行う。
In the above-mentioned apparatus, when there is no interference wave, the output of the detector 11 is applied to the drive circuit 16 as shown in the figure, and the switch 7 is first opened for observation.

すなわち空中線1,2の出力が互に90度の位相差を有
する低周波信号で平衡変調されて、その変調出力が合成
されるから、上記空中線を直接回転した場合と同様の効
果が得られる。
That is, the outputs of the antennas 1 and 2 are balanced modulated with low frequency signals having a phase difference of 90 degrees, and the modulated outputs are combined, so that the same effect as when the antennas are directly rotated can be obtained.

従ってこの出力を増幅、検波し、基準位相の上記低周波
信号と共に駆動回路16を介してブラウン管17の水平
並びに垂直偏向板に加えると、周知のようにプロペラ状
の図形が画かれる。
Therefore, when this output is amplified, detected, and applied to the horizontal and vertical deflection plates of the cathode ray tube 17 through the drive circuit 16 together with the low frequency signal of the reference phase, a propeller-shaped figure is drawn as is well known.

つぎにスイッチ7を閉成して、無指向性空中線の出力を
90度移相した信号を更に合成すると共に1駆動回路1
6において、前記低周波信号をブラウン管17の電子線
制御格子に加えるとバート形の図形が偏心的に現れてセ
ンスの指示が行われる。
Next, the switch 7 is closed, and the signal obtained by shifting the output of the omnidirectional antenna by 90 degrees is further synthesized, and the 1 drive circuit 1
At step 6, when the low frequency signal is applied to the electron beam control grid of the cathode ray tube 17, a bart-shaped figure appears eccentrically and a sense instruction is given.

このため前記プロペラ状の図形とこのセンスとによって
周知のように電波の到来方向を知ることができる。
Therefore, as is well known, the direction of arrival of radio waves can be determined by the propeller-shaped figure and this sense.

しかしこのような従来の装置においては、2つの電波が
混信している場合に各電波の到来方向を電波の強度比に
応じて合成した一方向だけが測定される。
However, in such a conventional device, when there is interference between two radio waves, only one direction is measured, which is obtained by combining the arrival directions of each radio wave according to the radio wave intensity ratio.

従ってこのような場合には、スイッチ15を切換えて検
波器14の出力を駆動回路16に加えると共にまずスイ
ッチ7を開放して観測を行う。
Therefore, in such a case, the switch 15 is switched to apply the output of the detector 14 to the drive circuit 16, and the switch 7 is first opened for observation.

すなわち2つの混信波の各々が単独に受信された場合に
、合成器6から送出される信号を第2図のaおよびbと
すると、該合成器はこれらを合成した信号を受信部10
に加える。
That is, if the signals sent out from the combiner 6 are a and b in FIG. 2 when each of the two interference waves is received individually, the combiner sends the combined signal to the receiver 10.
Add to.

帯域除去P波器12は検波器11の出力に含まれる低周
波分を除去するから、同調増幅器13には唸周波成分の
信号のみが加わる。
Since the band-removing P-wave device 12 removes the low frequency component contained in the output of the detector 11, only the signal of the beat frequency component is applied to the tuned amplifier 13.

従って増幅器13の同調周波数を適当に調整すると、2
つの混信波の差の周波数を有する第2図Cのような信号
が増幅され、検波器14で検波されてブラウン管駆動回
路16に加わる。
Therefore, if the tuning frequency of the amplifier 13 is adjusted appropriately, 2
A signal as shown in FIG. 2C having a frequency equal to the difference between the two interference waves is amplified, detected by the wave detector 14, and applied to the cathode ray tube drive circuit 16.

このため第1図のブラウン管17には、図に示したよう
に2つのプロペラ状の図形p、qが画かれて、各図形に
より前記2つの混信波の各々の到来方向またはこれと逆
の方向が指示される。
For this reason, two propeller-shaped figures p and q are drawn on the cathode ray tube 17 in FIG. is instructed.

従って次にスイッチ7を閉成すると、第2図a。Therefore, when switch 7 is then closed, FIG. 2a.

bの信号はd、eのように変化し、またCの信号はfの
ように変化する。
The signal b changes like d and e, and the signal C changes like f.

この信号fが検波されて駆動回路16に加わるから、該
7駆動回路によって更に発振器5から得られる基準低周
波信号でブラウン管の電子線制御格子の電位を制御する
と、第3図aまたはbに実線で示したようなバート形の
図形x、yが偏心的に画かれて前記プロペラ状図形p、
qのセンス指示が行われる。
Since this signal f is detected and applied to the drive circuit 16, when the potential of the electron beam control grid of the cathode ray tube is controlled by the reference low frequency signal obtained from the oscillator 5 by the seven drive circuits, the solid line in FIG. The bart-shaped figures x and y shown in are eccentrically drawn to form the propeller-shaped figure p,
A sense instruction for q is given.

すなわちこのセンス指示によって第3図aの場合は2つ
の混信波の到来方向がそれぞれ矢印Sおよびtであり、
またbの場合はSおよびUであることを知り得る。
That is, with this sense instruction, in the case of FIG. 3a, the arrival directions of the two interference waves are respectively arrows S and t, and
Also, in the case of b, it can be known that they are S and U.

このように本発明の装置は、複数の混信波がある場合に
その唸周波の信号を選択して増幅することによって電波
の到来方向を検出するものである。
As described above, the device of the present invention detects the arrival direction of radio waves by selecting and amplifying the signal of the beat frequency when there are a plurality of interference waves.

すなわち唸周波の信号は、第2図Cのように各受信波の
信号a、bの何れか一方の振幅が零になる時点でその振
幅が零になる。
In other words, the amplitude of the beat frequency signal becomes zero at the point in time when the amplitude of either one of the received wave signals a and b becomes zero, as shown in FIG. 2C.

従って唸周波信号を検波した出力が零になる位相を検出
することによって、各電波の到来方向を分別して検出す
ることができる。
Therefore, by detecting the phase at which the output of the detected beat frequency signal becomes zero, the direction of arrival of each radio wave can be detected separately.

このため本発明によって混信による大きな誤観測を防止
し得ると共に2つの電波の到来方向を同時に観測するこ
とができる。
Therefore, according to the present invention, large erroneous observations due to interference can be prevented, and the arrival directions of two radio waves can be observed simultaneously.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明の一実施例の構成を示した図、第2図は
第1図の装置の動作を説明する波形図、第3図は第1図
の装置によって表示される図形を示した図である。 なお図において、1,2は指向性空中線、3,4は平衡
変調器、5は低周波発振器、6は合成器、7はスイッチ
、8は無指向性空中線、9は90度移相器、10は受信
部、11は検波器、12は帯域除去済波器、13は同調
増幅器、14は検波器、15は切換スイッチ、16はブ
ラウン管1駆動回路、17はブラウン管である。
FIG. 1 is a diagram showing the configuration of an embodiment of the present invention, FIG. 2 is a waveform diagram explaining the operation of the device in FIG. 1, and FIG. 3 is a diagram showing figures displayed by the device in FIG. 1. This is a diagram. In the figure, 1 and 2 are directional antennas, 3 and 4 are balanced modulators, 5 is a low frequency oscillator, 6 is a combiner, 7 is a switch, 8 is an omnidirectional antenna, 9 is a 90 degree phase shifter, 10 is a receiving section, 11 is a wave detector, 12 is a band-removed wave detector, 13 is a tuning amplifier, 14 is a wave detector, 15 is a changeover switch, 16 is a cathode ray tube 1 drive circuit, and 17 is a cathode ray tube.

Claims (1)

【特許請求の範囲】[Claims] 1 指向性を機械的または電気的に回転する空中線の平
衡変調された出力の上記回転周期に対する位相を検出し
て電波の到来方向を求める方向探知機において、複数の
混信波が受信される場合にそれらの唸周波信号を増幅し
て検波する手段と、上記検波出力の振幅が零になる位相
を検出する手段とよりなる混信波方向分別装置。
1. When multiple interference waves are received in a direction finder that determines the arrival direction of radio waves by detecting the phase with respect to the rotation period of the balanced modulated output of an antenna whose directivity is mechanically or electrically rotated, An interference wave direction separation device comprising means for amplifying and detecting these beat frequency signals, and means for detecting a phase at which the amplitude of the detected output becomes zero.
JP10441180A 1980-07-31 1980-07-31 Interference wave direction separation device for direction finder Expired JPS5926909B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10441180A JPS5926909B2 (en) 1980-07-31 1980-07-31 Interference wave direction separation device for direction finder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10441180A JPS5926909B2 (en) 1980-07-31 1980-07-31 Interference wave direction separation device for direction finder

Publications (2)

Publication Number Publication Date
JPS5729967A JPS5729967A (en) 1982-02-18
JPS5926909B2 true JPS5926909B2 (en) 1984-07-02

Family

ID=14379956

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10441180A Expired JPS5926909B2 (en) 1980-07-31 1980-07-31 Interference wave direction separation device for direction finder

Country Status (1)

Country Link
JP (1) JPS5926909B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6299952U (en) * 1985-12-12 1987-06-25

Also Published As

Publication number Publication date
JPS5729967A (en) 1982-02-18

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