JPS6352713B2 - - Google Patents

Info

Publication number
JPS6352713B2
JPS6352713B2 JP13622782A JP13622782A JPS6352713B2 JP S6352713 B2 JPS6352713 B2 JP S6352713B2 JP 13622782 A JP13622782 A JP 13622782A JP 13622782 A JP13622782 A JP 13622782A JP S6352713 B2 JPS6352713 B2 JP S6352713B2
Authority
JP
Japan
Prior art keywords
phase
wave
signal
output
signals
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
JP13622782A
Other languages
Japanese (ja)
Other versions
JPS5927273A (en
Inventor
Takeshi Yasuda
Yukio Saito
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 JP13622782A priority Critical patent/JPS5927273A/en
Publication of JPS5927273A publication Critical patent/JPS5927273A/en
Publication of JPS6352713B2 publication Critical patent/JPS6352713B2/ja
Granted 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four

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)

Description

【発明の詳細な説明】 従来の方向探知機は受信電波に一定の低周波信
号で振幅変調を加えて、上記電波の到来方向を観
測していた。しかし受信波の周波数がVHF帯以
上になると、位相または周波数変調を利用するこ
とによつて雑音による精度の低下を防止すること
ができると共に安定性も向上する。本発明はこの
ような方式の方向探知機において、更に雑音の影
響を除去することにより精度を一層向上すると共
に安定に動作するようにしたものである。
DETAILED DESCRIPTION OF THE INVENTION A conventional direction finder subjects a received radio wave to amplitude modulation with a constant low frequency signal to observe the direction of arrival of the radio wave. However, when the frequency of the received wave exceeds the VHF band, by using phase or frequency modulation, it is possible to prevent a decrease in accuracy due to noise and improve stability. The present invention further improves the accuracy and stabilizes operation of such a direction finder by further eliminating the influence of noise.

第1図は本発明実施例の構成図で、互に直交す
るように配置された枠型空中線1,2の出力を平
衡変調器3,4に加えて矩形波信号発生器5の出
力S,Cで変調し、その平衡変調器の出力および
無指向性の垂直空中線6の出力を合成回路7で合
成してある。この合成出力を高周波増幅器8、中
間周波増幅器9等で増幅し、振幅制限器10を介
して周波数弁別器11に加えてある。また前記信
号発生器5の出力S,Cは第2図に示したように
互に90度の位相差を有する例えば133Hzの矩形波
であるが、この出力を信号変換器12に加えて
a,b,c,dおよびA,B,,のようなス
イツチ制御信号を得ている。
FIG. 1 is a block diagram of an embodiment of the present invention, in which the outputs of frame antennas 1 and 2 arranged orthogonally to each other are applied to balanced modulators 3 and 4, and the outputs S of a rectangular wave signal generator 5, The output of the balanced modulator and the output of the omnidirectional vertical antenna 6 are combined by a combining circuit 7. This combined output is amplified by a high frequency amplifier 8, an intermediate frequency amplifier 9, etc., and is applied to a frequency discriminator 11 via an amplitude limiter 10. The outputs S and C of the signal generator 5 are, for example, 133Hz rectangular waves having a phase difference of 90 degrees as shown in FIG. Switch control signals such as b, c, d and A, B, . are obtained.

第3図は前記枠型空中線1,2の平面図で、矢
印pの方向から電波が到来するものとすると各空
中線にはそれぞれoqおよびorの長さに比例した出
力が発生する。この出力が平衡変調器3,4で信
号SおよびCによつて変調されるから、第2図に
MsおよびMcで示したような信号が得られる。す
なわち信号Ms,Mcの振幅は上記oq,orに比例
し、高周波成分の極性が実線部分および点線部分
で示したように信号S,Cの正負によつて反転す
る。また垂直空中線6は枠型空中線1,2と90度
の位相差を有する信号Lを送出するが、これを移
相することなく直接合成回路7に加えてある。従
つてこの信号Lは第2図に破線部分で表わしたよ
うに信号Ms,Mcの実線部分および点線部分の何
れに対しても90度の位相差を有し、合成回路7は
上記信号Ms,McおよびLを合成して、Hのよう
な信号を送出する。すなわち信号Lの高周波成分
に対して、信号Ms,Mcの実線部分は90度の進み
位相を有し、点線部分は90度の遅れ位相であると
すると、信号Ms,Mcが共に進み位相の部分では
信号Hの位相が大巾に進み位相となり、共に遅れ
位相の部分では大巾に遅れ位相となる。また信号
Ms,Mcの一方が進み位相他方が遅れ位相の部分
では、該信号Ms,Mcの大小に応じて信号Hが信
号Lより適当な進みまたは遅れ位相となる。かつ
このような位相の変動は矩形低周波信号Sおよび
Cの上昇および下降時点のみで発生して、進み位
相となる過程では高周波信号の周波数が実質的に
低下し遅れ位相となる過程では上昇する。このた
め第1図のように、高周波並びに中間周波増幅器
8,9および振幅制限器10を介して合成回路7
の出力を周波数弁別器11に加えると第2図にF
で示したような検波出力信号が得られる。
FIG. 3 is a plan view of the frame-shaped antennas 1 and 2. If radio waves arrive from the direction of arrow p, each antenna generates an output proportional to the lengths o q and o r , respectively. Since this output is modulated by the signals S and C in the balanced modulators 3 and 4, as shown in FIG.
Signals as shown by Ms and Mc are obtained. That is, the amplitudes of the signals Ms and Mc are proportional to the above o q and o r , and the polarity of the high frequency component is reversed depending on the sign of the signals S and C, as shown by the solid line and dotted line. Further, the vertical antenna 6 sends out a signal L having a phase difference of 90 degrees from the frame antennas 1 and 2, but this is directly added to the synthesis circuit 7 without phase shifting. Therefore, this signal L has a phase difference of 90 degrees with respect to both the solid line part and the dotted line part of the signals Ms and Mc, as shown by the broken line part in FIG. Combine Mc and L and send out a signal like H. In other words, with respect to the high frequency component of the signal L, the solid line portion of the signals Ms and Mc has a 90 degree lead phase, and the dotted line portion has a 90 degree lag phase, then the part where the signals Ms and Mc both have a lead phase In this case, the phase of the signal H advances by a large width and becomes a phase, and the phase of the signal H becomes a phase that lags by a wide range. Also the signal
In a portion where one of Ms and Mc is in a leading phase and the other is in a lagging phase, the signal H has an appropriate leading or lagging phase than the signal L depending on the magnitude of the signals Ms and Mc. Moreover, such phase fluctuations occur only at the rising and falling points of the rectangular low-frequency signals S and C, and the frequency of the high-frequency signal substantially decreases in the process of leading phase and increases in the process of lagging phase. . For this reason, as shown in FIG.
When the output of F is added to the frequency discriminator 11, it becomes F
The detection output signal shown in is obtained.

第1図のようにスイツチ回路13,14,1
5,16を介して上記信号Fを記憶回路17,1
8,19,20に加え、更にスイツチ回路21,
22,23,24を介して各記憶回路の出力を加
算回路25に加えてある。スイツチ回路13〜1
6は前記信号a,b,c,dを加えられたときだ
けそれぞれ短時間あて閉成するから、記憶回路1
7には信号F中のパルスFaがサンプリングされ
てその振幅wが第2図にMaで示したように記憶
され、また記憶回路18,19,20にはそのパ
ルスFb,Fc,Fdをサンプリングした振幅x,
y,zがMb,Mc,Mdのように記憶される。更
にスイツチ回路21〜24は信号A,B,およ
びによつて閉成するから、加算回路25には記
憶回路17〜20の出力Ma,Mb,Mc,Mdが
信号S,Cの4分の1周期毎に順次2つ宛加えら
れてそれらの和が送出される。すなわちスイツチ
回路21と22とが閉成する期間においては記憶
回路17,18の出力wおよびxが加算回路25
に加えられて、その和が送出され、次に22と2
3が閉成すると記憶回路18,19の出力xおよ
びyが加算回路25に加えられてその和が送出さ
れる。このような動作によつて加算回路25は第
2図にGで示したような階段波信号を送出する。
従つて第1図のように上記信号Gを、矩形波S,
C等の基本波成分を抽出するフイルタ26に加え
ると、第2図にKで示したような正弦波形の出力
が得られる。この信号Kを前記信号変換器12か
ら得られる基準位相信号と共に位相検出器27に
加えて位相φを検出し、表示器28によつて第3
図に矢印pで示したような電波の到来方位角θを
表示させる。すなわち上記方位角θによつて第2
図における平衡変調信号Ms,Mcの振幅が定ま
り、この振幅によつて同図Fにおける各パルスの
振幅w,x,y,zが定まる。階段波Gはその振
幅w,x,y,zを矩形変調波S,Cの4分の1
周期毎に加算して得たものである。従つてこの階
段波Gに含まれる基本波成分Kを抽出すると、そ
の位相角φが電波の到来方位角qに対応する。
As shown in Figure 1, switch circuits 13, 14, 1
5, 16 to the storage circuits 17, 1.
In addition to 8, 19, 20, switch circuits 21,
The outputs of each memory circuit are added to an adder circuit 25 via 22, 23, and 24. Switch circuit 13-1
6 is applied and closed for a short time only when the signals a, b, c, and d are applied, so that the memory circuit 1
7, the pulse Fa in the signal F is sampled and its amplitude w is stored as shown by Ma in FIG. amplitude x,
y, z are stored as Mb, Mc, Md. Further, since the switch circuits 21 to 24 are closed by the signals A, B, and the outputs Ma, Mb, Mc, and Md of the memory circuits 17 to 20 are sent to the adder circuit 25, the outputs Ma, Mb, Mc, and Md are one quarter of the signals S and C. Two addresses are sequentially added every cycle and the sum is sent out. That is, during the period when the switch circuits 21 and 22 are closed, the outputs w and x of the memory circuits 17 and 18 are output to the adder circuit 25.
, the sum is sent out, and then 22 and 2
3 is closed, the outputs x and y of the memory circuits 18 and 19 are added to the adder circuit 25, and the sum thereof is sent out. Through this operation, the adder circuit 25 sends out a staircase wave signal as shown by G in FIG.
Therefore, as shown in FIG. 1, the signal G is converted into a rectangular wave S,
When the fundamental wave component such as C is added to the filter 26 for extracting it, a sinusoidal waveform output as shown by K in FIG. 2 is obtained. This signal K is applied to the phase detector 27 together with the reference phase signal obtained from the signal converter 12 to detect the phase φ.
The arrival azimuth θ of the radio waves as shown by the arrow p in the figure is displayed. That is, by the above azimuth angle θ, the second
The amplitudes of the balanced modulation signals Ms and Mc in the figure are determined, and the amplitudes w, x, y, and z of each pulse in the figure F are determined by these amplitudes. The staircase wave G has its amplitude w, x, y, z a quarter of that of the rectangular modulated waves S, C.
It is obtained by adding each cycle. Therefore, when the fundamental wave component K included in the staircase wave G is extracted, its phase angle φ corresponds to the arrival azimuth q of the radio wave.

以上実施例について説明したように本発明の方
向探知機は矩形波の低周波変調信号S,Cを用
い、枠型空中線出力をこの信号S,Cで平衡変調
した出力に無指向性の垂直空中線の出力を直接合
成して電波の到来方向に対応した位相変調波を形
成することにより、その周波数変調成分を信号
S,Cの上昇、下降部分に集中させてある。この
信号の周波数弁別によりパルス信号Fを得て、各
パルスの振幅を信号S,Cの4分の1周期毎に順
次加算することにより前記位相変調波に相当する
階段波を形成し、その基本波成分の位相を検出し
て電波の到来方向を知るものである。すなわち方
位情報を矩形波の上昇、下降部分のみに集中させ
て、この部分の情報のみをサンプリングするか
ら、上記矩形波の平担部分に含まれる種々の雑音
成分の影響による精度低下を防止して精密な測定
を行うことができる。しかも前記パルスの振幅を
4分の1周期毎に2つ宛加算して階段波を形成
し、その基本波を抽出して位相の検出を行うか
ら、充分大きな出力が得られて、高感度で安定に
動作する。また電波に音声その他の信号が含まれ
ている場合でも、信号S,Cの上昇下降部分にお
ける周波数変調成分とこれに隣接する部分の周波
数変調成分との差を得て、前述の処理を施すこと
により、上記音声信号等による誤差も容易に防止
される。
As explained in the embodiments above, the direction finder of the present invention uses rectangular wave low-frequency modulation signals S and C, and uses the signals S and C to balance-modulate the frame-shaped antenna output. By directly combining the outputs of the signals to form a phase modulated wave corresponding to the arrival direction of the radio waves, the frequency modulation components are concentrated in the rising and falling portions of the signals S and C. A pulse signal F is obtained by frequency discrimination of this signal, and by sequentially adding the amplitude of each pulse every quarter period of the signals S and C, a staircase wave corresponding to the phase modulated wave is formed, and its basic The direction of arrival of radio waves can be determined by detecting the phase of the wave components. In other words, since the azimuth information is concentrated only on the rising and falling parts of the rectangular wave and only the information in these parts is sampled, it is possible to prevent a decrease in accuracy due to the effects of various noise components included in the flat part of the rectangular wave. Precise measurements can be made. Moreover, the amplitudes of the pulses are added two times every quarter cycle to form a staircase wave, and the fundamental wave is extracted to detect the phase, so a sufficiently large output can be obtained and high sensitivity can be obtained. Operates stably. Furthermore, even if the radio waves contain audio or other signals, the difference between the frequency modulation components in the rising and falling parts of the signals S and C and the frequency modulation components in the adjacent parts can be obtained and the above-mentioned processing can be performed. Therefore, errors caused by the audio signal and the like can be easily prevented.

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

第1図は本発明実施例の構成図、第2図は第1
図における各部の信号波形図、第3図は第1図の
一部の平面図である。なお図において、1,2は
枠型空中線、3,4は平衡変調器、5は信号発生
器、6は垂直空中線、7は合成回路、8は高周波
増幅器、9は中間周波増幅器、10は振幅制限
器、11は周波数弁別器、12は信号変換器、1
3,14,15,16はスイツチ回路、17,1
8,19,20は記憶回路、21,22,23,
24はスイツチ回路、25は加算回路、26はフ
イルタ、27は位相検出器、28は表示器であ
る。
Figure 1 is a configuration diagram of an embodiment of the present invention, and Figure 2 is a diagram of the first embodiment.
FIG. 3 is a plan view of a part of FIG. 1. In the figure, 1 and 2 are frame antennas, 3 and 4 are balanced modulators, 5 is a signal generator, 6 is a vertical antenna, 7 is a combining circuit, 8 is a high frequency amplifier, 9 is an intermediate frequency amplifier, and 10 is an amplitude limiter, 11 is a frequency discriminator, 12 is a signal converter, 1
3, 14, 15, 16 are switch circuits, 17, 1
8, 19, 20 are memory circuits, 21, 22, 23,
24 is a switch circuit, 25 is an adder circuit, 26 is a filter, 27 is a phase detector, and 28 is a display.

Claims (1)

【特許請求の範囲】[Claims] 1 指向性が互に直交する1対の空中線の出力を
互に90度の位相差を有する2つの矩形波でそれぞ
れ平衡変調して無指向性の空中線出力に合成する
装置と、上記合成装置の出力を増幅して周波数弁
別を行う装置と、上記周波数弁別装置の出力を前
記2つの矩形波における各々の上昇並びに下降時
点毎にサンプリングしてそのサンプリング値をそ
れぞれ記憶する装置と、上記各記憶装置の出力を
前記矩形波の4分の1周期毎に順次2つ宛加算し
て1つの階段波となしかつその階段波に含まれる
基本正弦波成分を得る装置と、上記基本正弦波成
分の位相を検出して電波の到来方向を表示する装
置とよりなることを特徴とする方向探知機。
1. A device that balance-modulates the outputs of a pair of antennas whose directivities are orthogonal to each other with two rectangular waves having a phase difference of 90 degrees and synthesizes them into an omnidirectional antenna output; a device that amplifies the output and performs frequency discrimination; a device that samples the output of the frequency discrimination device at each rise and fall point in the two rectangular waves and stores the sampled values; and each of the storage devices mentioned above. A device for sequentially adding two outputs of the rectangular wave every quarter period of the rectangular wave to form one staircase wave and obtaining a fundamental sine wave component included in the staircase wave, and a phase of the fundamental sine wave component. What is claimed is: 1. A direction finder comprising: a device that detects and displays the direction of arrival of radio waves;
JP13622782A 1982-08-06 1982-08-06 Direction finder Granted JPS5927273A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13622782A JPS5927273A (en) 1982-08-06 1982-08-06 Direction finder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13622782A JPS5927273A (en) 1982-08-06 1982-08-06 Direction finder

Publications (2)

Publication Number Publication Date
JPS5927273A JPS5927273A (en) 1984-02-13
JPS6352713B2 true JPS6352713B2 (en) 1988-10-19

Family

ID=15170255

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13622782A Granted JPS5927273A (en) 1982-08-06 1982-08-06 Direction finder

Country Status (1)

Country Link
JP (1) JPS5927273A (en)

Also Published As

Publication number Publication date
JPS5927273A (en) 1984-02-13

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