JPS6010269B2 - direction finder - Google Patents

direction finder

Info

Publication number
JPS6010269B2
JPS6010269B2 JP11449081A JP11449081A JPS6010269B2 JP S6010269 B2 JPS6010269 B2 JP S6010269B2 JP 11449081 A JP11449081 A JP 11449081A JP 11449081 A JP11449081 A JP 11449081A JP S6010269 B2 JPS6010269 B2 JP S6010269B2
Authority
JP
Japan
Prior art keywords
circuit
phase shift
output
antenna
outputs
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
JP11449081A
Other languages
Japanese (ja)
Other versions
JPS5817381A (en
Inventor
憲三 森
幸雄 斉藤
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 JP11449081A priority Critical patent/JPS6010269B2/en
Publication of JPS5817381A publication Critical patent/JPS5817381A/en
Publication of JPS6010269B2 publication Critical patent/JPS6010269B2/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

Description

【発明の詳細な説明】 指向性のある枠型空中線あるいはアドコツク空中線等と
無指向性の垂直空中線とを用いた方向探知機において従
釆は一般に無指向性空中線の出力のみを1つの90度移
相器に加えて指向性空中線の出力と合成していた。
DETAILED DESCRIPTION OF THE INVENTION In a direction finder that uses a directional frame antenna or an adkotok antenna and an omnidirectional vertical antenna, the follower generally moves only the output of the omnidirectional antenna by one 90 degrees. In addition to the phase box, it was combined with the output of the directional antenna.

しかしこのような方向探知機は、移相器の出力が周波数
によって変化するために、例えば枠型空中線を用いた場
合においては受信周波数が低いときセンス決定比、すな
わち垂直空中線出力と指向性空中線出力との比が4・さ
くなってセンス不鮮明および感度低下を生ずる。また受
信周波数が高くなると逆にセンス決定比の過大によって
センスが不鮮明となる欠点があり、このような欠点を除
くために複雑な回路を必要とした。従って本発明は簡単
な構成によって上述のような欠点のない方向探知機を提
供するものである。第1図は本発明実施例の構成を示し
た図で、指向性が互に直交するように配置された2つの
枠型空中線1,2にそれぞれ変成器3,4を介して2芯
ケーブル5,6の一端を接続してある。
However, in such a direction finder, since the output of the phase shifter changes depending on the frequency, for example, when using a frame antenna, when the reception frequency is low, the sense determination ratio, that is, the vertical antenna output and the directional antenna output The ratio between the two images decreases by 4.0, resulting in blurred sense and decreased sensitivity. Furthermore, as the reception frequency increases, there is a drawback that the sensing becomes unclear due to an excessive sense determination ratio, and a complicated circuit is required to eliminate this drawback. Therefore, the present invention provides a direction finder which is simple in construction and free from the above-mentioned drawbacks. FIG. 1 is a diagram showing the configuration of an embodiment of the present invention, in which a two-core cable 5 is connected to two frame-shaped antennas 1 and 2, which are arranged so that their directivities are orthogonal to each other, via transformers 3 and 4, respectively. , 6 are connected.

また変成器3,4の一次巻線の中性点を接続して、この
接続部と大地との間に枠型空中線1,2と等しいィンダ
クタンスの線論7を直列に挿入し、その線輪の両端間に
変成器3,4と同一特性の変成器8を介してケーブル5
,6と同一の2芯ケーブル9を接続してある。すなわち
枠型空中線1,2を、その高さに相当するセンス決定用
の垂直空中線として兼用したもので、この垂直空中線お
よび前記枠型空中線の出力インピーダンスが一致し、か
つそれらの出力が同一特性のケーブル5,6および9で
伝送される。従ってこのケーブルで各空中線の出力を受
信装置10に導くことにより、信号の位相並びに振幅の
関係を一定に保つことができる。受信装置1川こおいて
は、ケーブル6,6の出力をそれぞれ平衡変調器1 1
,12に加えて、例えば13班gの低周波発振器13の
出力で変調してある。
In addition, the neutral points of the primary windings of the transformers 3 and 4 are connected, and a line 7 having the same inductance as the frame antennas 1 and 2 is inserted in series between this connection and the ground. A cable 5 is connected between both ends of the ring via a transformer 8 having the same characteristics as the transformers 3 and 4.
, 6 are connected to the same two-core cable 9. That is, the frame-shaped antennas 1 and 2 are also used as vertical antennas for determining the sense corresponding to the height thereof, and the output impedance of this vertical antenna and the frame-shaped antenna are the same, and their outputs have the same characteristics. Transmitted on cables 5, 6 and 9. Therefore, by guiding the output of each antenna to the receiving device 10 using this cable, the relationship between the phase and amplitude of the signals can be kept constant. In the receiving device 1, the outputs of the cables 6 and 6 are connected to balanced modulators 1 and 1, respectively.
.

なお発振器13から変調器11,12に加える変調波に
は互に90度の位相差を与え、各変調器の出力を合成し
て移相回路14に加えてある。またケーブル9の出力は
、平衡変調器11,12と等価の入出力特性を有する等
価回路15を介して移相回路16に加えられる。上記2
つの移相回路14,16の出力を合成して、増幅器17
で増幅し、その出力を検波器18に加えて前記13班g
の低周波信号を復調する。この再生された低周波信号を
発振器13から得られる基準位相信号と共に位相測定回
路19に加えて、その位相を検出することにより電波の
到釆方向を知ることができる。第2図a,bはそれぞれ
第1図における移相回路14,16の回路例で、電界効
果トランジスタFETに容量性リアクタンス×cと抵抗
Rまたは誘導性リアクタンスXIと抵抗Rをそれぞれ直
列に接続して、その接続部を出力端子C、またはトラン
ジスタのゲートを入力端子1としてある。
The modulated waves applied from the oscillator 13 to the modulators 11 and 12 are given a phase difference of 90 degrees, and the outputs of the respective modulators are combined and applied to the phase shift circuit 14. Further, the output of the cable 9 is applied to a phase shift circuit 16 via an equivalent circuit 15 having input/output characteristics equivalent to those of the balanced modulators 11 and 12. Above 2
The outputs of the two phase shift circuits 14 and 16 are combined and the amplifier 17
The output is amplified by the detector 18 and the 13 groups g
demodulates the low frequency signal. By applying this reproduced low frequency signal to the phase measuring circuit 19 together with the reference phase signal obtained from the oscillator 13 and detecting the phase, the arrival direction of the radio wave can be determined. Figures 2a and 2b are circuit examples of the phase shift circuits 14 and 16 in Figure 1, respectively, in which a capacitive reactance xc and a resistor R or an inductive reactance XI and a resistor R are connected in series to a field effect transistor FET. The connection part is set as the output terminal C, or the gate of the transistor is set as the input terminal 1.

従ってトランジスタFETの増幅率を〃、内部抵抗をy
、また回路aおよびbにおける端子1の入力をそれぞれ
e,,ev、端子○の出力をE,,Evとすると、が成
立する。
Therefore, the amplification factor of the transistor FET is 〃, and the internal resistance is y
, and let the inputs of terminals 1 in circuits a and b be e, ev, respectively, and the outputs of terminals ○ be E, ev, then the following holds true.

よって×c・×,=(R+y)2となるようにIJァク
タンスXc,XIおよび抵抗Rを選定すると、EV r=−i舎・単ユ......【3, E, X. が得られる。
Therefore, if the IJ factors Xc, XI and the resistance R are selected so that xc. .. .. .. .. .. [3, E, X. is obtained.

このように第1図の移相回路14,16はその総合移相
量が周波数に関係なく常に90度となる相補性を有する
。また上記第{3’式において枠型空中線の出力e,は
受信電波の周波数に比例して、垂直空中線の出力evは
周波数の2乗に比例し、かつリアクタンス×,は周波数
に比例するから、結局移相回路14,16の出力の比I
Ev/B,lは周波数に関係なく一定の値となる。すな
わちセンス決定比が受信周波数によって変化しないから
、el,evを予め適当に設定しておくことにより、受
信電波の周波数変化に関係なく、常に明確なセンス決定
が行われる。なお第3図a,bは移相回路14,16の
他の例で、各部の符号は第2図と同一である。
In this way, the phase shift circuits 14 and 16 shown in FIG. 1 have complementarity so that their total phase shift amount is always 90 degrees regardless of the frequency. In addition, in the {3'th equation above, the output e of the frame antenna is proportional to the frequency of the received radio wave, the output ev of the vertical antenna is proportional to the square of the frequency, and the reactance x is proportional to the frequency. In the end, the ratio I of the outputs of the phase shift circuits 14 and 16
Ev/B,l takes a constant value regardless of frequency. That is, since the sense determination ratio does not change depending on the receiving frequency, by setting el and ev appropriately in advance, a clear sense determination can always be made regardless of changes in the frequency of the received radio waves. Note that FIGS. 3a and 3b show other examples of the phase shift circuits 14 and 16, and the reference numerals of each part are the same as in FIG. 2.

すなわちこの回路においてはが成立し、これらによって
前記第‘3}式が得られる。
That is, in this circuit, the following holds true, and the above-mentioned equation '3' can be obtained from these.

従って第3図の移相回路も相補性を有し、かつセンス決
定比を周波数に関係なく一定に保つことができる。上述
のように移相器14,16は、枠型空中線1,2の出力
に正の移相推移を与え、垂直空中線に負の移相推移を与
えて、その移相量の和が周波数に関係なく常に90度と
なるようにしたもので、この出力が合成されて増幅器1
7を介し検波器18で復調される。
Therefore, the phase shift circuit of FIG. 3 also has complementarity and can keep the sense determination ratio constant regardless of frequency. As mentioned above, the phase shifters 14 and 16 give a positive phase shift to the outputs of the frame antennas 1 and 2, and a negative phase shift to the vertical antenna, so that the sum of the phase shifts becomes the frequency. The angle is always 90 degrees regardless of the angle, and this output is combined and sent to amplifier 1.
7 and is demodulated by a detector 18.

従って位相測定回路19で復調波の位相を検出すること
によって、受信電波の到来方向を測定することができる
。なお第1図の実施例は、枠型空中線1,2の出力を互
に90度の位相差を有する低周波信号で平衡変調して、
その復調波の位相により電波の到来方向を測定したもの
であるが、例えば枠型空中線1,2の出力をゴニオメー
タに加えて、サーボ機構でそのゴニオメータを駆動する
ことにより方位測定を行うこと等も可能である。また低
周波による変調は、これを垂直空中線の出力に加えるこ
ともできると共に枠型空中線と別個に独立の垂直空中線
を設けることも勿論可能である。更に指向性空中線とし
てアドコック空中線を用いることもできるが、この場合
出力回路の構成によってはセンス決定比が周波数に逆比
例することがある。このような場合は第2図、第3図の
相補性移相回路a,bを逆に用いることによって同機の
効果が得られる。以上説明したように本発明は総合移相
量が周波数に関係なく常に90度となる1対の相補性移
相回路を介して合成するもので、受信電波の周波数に関
係なく、しかも複雑な回路等を必要とすることなく常に
鮮明なセンス決定を行うことができる。
Therefore, by detecting the phase of the demodulated wave with the phase measuring circuit 19, the arrival direction of the received radio wave can be measured. In the embodiment shown in FIG. 1, the outputs of the frame antennas 1 and 2 are balanced-modulated with low-frequency signals having a phase difference of 90 degrees.
The direction of arrival of the radio wave is measured based on the phase of the demodulated wave, but it is also possible to measure the direction by, for example, adding the outputs of the frame antennas 1 and 2 to a goniometer and driving the goniometer with a servo mechanism. It is possible. Furthermore, low frequency modulation can be added to the output of the vertical antenna, and it is of course also possible to provide an independent vertical antenna separately from the frame antenna. Furthermore, an Adcock antenna can be used as the directional antenna, but in this case, depending on the configuration of the output circuit, the sense determination ratio may be inversely proportional to the frequency. In such a case, the same effect can be obtained by using the complementary phase shift circuits a and b shown in FIGS. 2 and 3 in reverse. As explained above, the present invention performs synthesis through a pair of complementary phase shift circuits such that the total phase shift amount is always 90 degrees regardless of the frequency, and it requires a complex circuit regardless of the frequency of the received radio waves. It is possible to always make clear sense decisions without the need for such things.

【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、第3図は第1
図の一部の回路例である。 なお図において、1,2は枠型空中線、3,4,8は変
成器、7は線輪、5,6,9はケーブル、1川ま受信装
置、11,12は平衡変調器、15は等価回路、13は
低周波発振器、14,16は相補性移相回略、17は増
幅器、18は検波器、19は位相測定回路である。オ/
鼠 次z優 ゲヲ亀
Figure 1 is a configuration diagram of an embodiment of the present invention, Figures 2 and 3 are
This is an example of a part of the circuit shown in the figure. In the figure, 1 and 2 are frame antennas, 3, 4, and 8 are transformers, 7 is a coil, 5, 6, and 9 are cables, 1 is a receiving device, 11 and 12 are balanced modulators, and 15 is a In the equivalent circuit, 13 is a low frequency oscillator, 14 and 16 are complementary phase shift circuits, 17 is an amplifier, 18 is a detector, and 19 is a phase measurement circuit. O/
Nezujiz Yugewokame

Claims (1)

【特許請求の範囲】[Claims] 1 指向性を有する空中線または無指向性垂直空中線の
出力の一方を低周波信号で変調する平衡変調器および該
変調器と等価の入出力特性を有し他方の出力を加えられ
る等価回路と、上記指向性空中線並びに無指向性垂直空
中線の出力をそれぞれ加えられて総合移相量が周波数に
関係なく常に90度となる1対の相補性移相回路と、前
記平衡変調器および相補性移相回路の一方並びに前記等
価回路および相補性移相回路の他方を通った指向性並び
に無指向性空中線の出力を合成して増幅する回路と、上
記増幅回路の出力を検波して前記低周波信号を復調する
回路とよりなることを特徴とする方向探知機。
1. A balanced modulator that modulates one of the outputs of a directional antenna or an omnidirectional vertical antenna with a low frequency signal, and an equivalent circuit that has input/output characteristics equivalent to that of the modulator and can add the output of the other, and the above-mentioned a pair of complementary phase shift circuits to which the outputs of a directional antenna and an omnidirectional vertical antenna are added so that the total phase shift amount is always 90 degrees regardless of frequency; the balanced modulator and the complementary phase shift circuit; a circuit that synthesizes and amplifies the outputs of the directional and omnidirectional antennas that have passed through one of the circuits and the other of the equivalent circuit and the complementary phase shift circuit; and a circuit that detects the output of the amplifier circuit and demodulates the low frequency signal. A direction finder characterized by a circuit for detecting
JP11449081A 1981-07-23 1981-07-23 direction finder Expired JPS6010269B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11449081A JPS6010269B2 (en) 1981-07-23 1981-07-23 direction finder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11449081A JPS6010269B2 (en) 1981-07-23 1981-07-23 direction finder

Publications (2)

Publication Number Publication Date
JPS5817381A JPS5817381A (en) 1983-02-01
JPS6010269B2 true JPS6010269B2 (en) 1985-03-15

Family

ID=14639054

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11449081A Expired JPS6010269B2 (en) 1981-07-23 1981-07-23 direction finder

Country Status (1)

Country Link
JP (1) JPS6010269B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180168629A1 (en) * 2016-12-21 2018-06-21 Ethicon Endo-Surgery, Llc Staple cartridges and arrangements of staples and staple cavities therein

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6080360U (en) * 1983-11-04 1985-06-04 株式会社光電製作所 Wireless direction finder with automatic selection of sense signal phase shift constant
JPS6092179U (en) * 1983-11-30 1985-06-24 株式会社光電製作所 Sense signal phase shift constant program selection method radio direction finder

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180168629A1 (en) * 2016-12-21 2018-06-21 Ethicon Endo-Surgery, Llc Staple cartridges and arrangements of staples and staple cavities therein

Also Published As

Publication number Publication date
JPS5817381A (en) 1983-02-01

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