JPH0449803B2 - - Google Patents

Info

Publication number
JPH0449803B2
JPH0449803B2 JP59130141A JP13014184A JPH0449803B2 JP H0449803 B2 JPH0449803 B2 JP H0449803B2 JP 59130141 A JP59130141 A JP 59130141A JP 13014184 A JP13014184 A JP 13014184A JP H0449803 B2 JPH0449803 B2 JP H0449803B2
Authority
JP
Japan
Prior art keywords
antenna element
output
antenna elements
phase
circuit
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 - Lifetime
Application number
JP59130141A
Other languages
Japanese (ja)
Other versions
JPS6110302A (en
Inventor
Kenzo Mori
Takeshi Yasuda
Minoru Suzuki
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 JP13014184A priority Critical patent/JPS6110302A/en
Publication of JPS6110302A publication Critical patent/JPS6110302A/en
Publication of JPH0449803B2 publication Critical patent/JPH0449803B2/ja
Granted legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/29Combinations of different interacting antenna units for giving a desired directional characteristic

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Description

【発明の詳細な説明】 地面と平行な水平アンテナの一端を接地して他
端から受信出力を取り出すと、電波の入射方向の
変化に応じてカージオイド曲線の感度特性が得ら
れる。従つてこのようなアンテナを用いて方向探
知機を得ることができるが、本発明は電子的切換
回路によつて電波の到来方向に対応した波形の出
力を得ると共に電波が弱い場合に雑音成分のため
に測定誤差が増大することを防止し、あるいは電
波の断続によつて受信機のAGC動作が完全に行
われないような場合でも正確な方位測定を行い得
るようにした空中線装置を提供するものである。
DETAILED DESCRIPTION OF THE INVENTION When one end of a horizontal antenna parallel to the ground is grounded and the reception output is taken out from the other end, a cardioid curve sensitivity characteristic is obtained in response to changes in the direction of incidence of radio waves. Therefore, a direction finder can be obtained using such an antenna, but the present invention uses an electronic switching circuit to obtain a waveform output corresponding to the arrival direction of the radio wave, and also to suppress the noise component when the radio wave is weak. To provide an antenna device that prevents measurement errors from increasing due to radio waves, or enables accurate azimuth measurement even when the AGC operation of a receiver is not completed due to intermittent radio waves. It is.

本発明は例えば飛行機の機体あるいは自動車の
屋根のように接地面とみなすことのできる導体板
上に複数個の帯状アンテナ素子をそれらの中央部
が互に絶縁されて交叉するように配置し、その各
アンテナ素子の両端を上記交叉角に相当する位相
差で交互に接地して他端から得られる出力を合成
すると共に、更に前記交叉部に1つの垂直アンテ
ナ素子を設けてこのアンテナ素子の出力を上記合
成出力に適宜の位相をもつて合成するようにした
ものである。従つてアンテナを回転する等の機械
的な可動部を必要とすることなく、上記合成出力
を振幅または位相検波をして得られる信号の位相
角によつて電波の到来方向を知ることができる。
かつ垂直アンテナ素子を設けることによつて合成
されたアンテナ出力が増大し、あるいは位相変調
出力を得ることができる。このため雑音による誤
差が軽減されて正確な方位測定を行い得ると共に
電波の断続によつてAGC回路が充分機能しない
場合等においても位相変調出力を利用して支障な
く方位測定を行うことができる。しかも垂直アン
テナ素子を帯状アンテナ素子の中心に配置するか
らその指向特性が乱されるようなおそれがないも
のである。
The present invention involves arranging a plurality of band-shaped antenna elements on a conductor plate that can be considered as a ground plane, such as the fuselage of an airplane or the roof of a car, so that their central portions are insulated from each other and intersecting each other. Both ends of each antenna element are grounded alternately with a phase difference corresponding to the above-mentioned crossing angle, and the outputs obtained from the other ends are combined, and one vertical antenna element is further provided at the crossing point to combine the outputs of this antenna element. The above-mentioned combined output is combined with an appropriate phase. Therefore, the arrival direction of the radio wave can be determined from the phase angle of the signal obtained by amplitude or phase detection of the above-mentioned combined output without requiring any mechanical movable part such as rotating the antenna.
In addition, by providing a vertical antenna element, the combined antenna output can be increased or a phase modulated output can be obtained. Therefore, errors due to noise are reduced and accurate direction measurement can be performed, and even in cases where the AGC circuit does not function sufficiently due to intermittent radio waves, direction measurement can be performed without any problem using the phase modulation output. Furthermore, since the vertical antenna element is arranged at the center of the strip antenna element, there is no fear that its directivity characteristics will be disturbed.

第1図は本発明実施例の縦断面図、第2図はそ
の一部を截欠した平面図で、導体板1は例えば飛
行機の機体あるいは自動車の屋根等である。この
導体板1に円孔2を設けて、その孔を塞いだ絶縁
体板3の内面に互に直交する2つの帯状アンテナ
素子4,5を取付けてある。これらのアンテナ素
子は巾が両端で次第に増大するように形成され
て、その中央の巾の狭い部分で互に接触しないよ
うに交叉している。また円孔2の内側には周縁が
導体板1に連結された浅い桶形の導体板6を設け
てその中央部に錐状の隆起部7を形成することに
より、実質的に接地されたこの導体板6とアンテ
ナ素子4,5との間の距離をそれらの巾に応じて
増大させてある。すなわちアンテナ素子4,5が
位置に関係なく一定の特性インピーダンスとなる
ようにしてある。なお上記導体板6の裏側には電
子的切換回路および各アンテナ出力の合成回路等
を収容した筐体8を取付けて、前記帯状アンテナ
素子4,5の両端を同軸ケーブル9,9…でこの
筐体内に導いてある。更に前記アンテナ素子4,
5の中央における交叉部に絶縁体板3の外部に突
出した垂直アンテナ素子10を設けて、その基部
を上記アンテナ素子に接触しないように筐体8内
に導いてある。なお筐体8には上記切換回路に加
えられる切換信号および必要な電源等を収容した
ケーブル11および前記各アンテナ素子の出力を
合成した信号を方向探知機の本体に導く同軸ケー
ブル12等を接続してある。
FIG. 1 is a longitudinal cross-sectional view of an embodiment of the present invention, and FIG. 2 is a partially cutaway plan view thereof. The conductor plate 1 is, for example, the fuselage of an airplane or the roof of an automobile. A circular hole 2 is provided in this conductor plate 1, and two band-shaped antenna elements 4 and 5 are attached to the inner surface of an insulator plate 3 which closes the hole and are perpendicular to each other. These antenna elements are formed so that their widths gradually increase at both ends, and intersect at the narrow center portions of the antenna elements so as not to touch each other. Furthermore, a shallow pail-shaped conductor plate 6 whose peripheral edge is connected to the conductor plate 1 is provided inside the circular hole 2, and a conical raised portion 7 is formed in the center of the conductor plate 6, so that this substantially grounded conductor plate 6 is provided. The distance between the conductor plate 6 and the antenna elements 4, 5 is increased according to their widths. That is, antenna elements 4 and 5 are designed to have a constant characteristic impedance regardless of their position. A housing 8 housing an electronic switching circuit, a combining circuit for each antenna output, etc. is attached to the back side of the conductor plate 6, and both ends of the band-shaped antenna elements 4, 5 are connected to this housing using coaxial cables 9, 9, . . . It is guided into the body. Furthermore, the antenna element 4,
A vertical antenna element 10 protruding to the outside of the insulator plate 3 is provided at the intersection at the center of the antenna element 5, and its base is guided into the housing 8 so as not to come into contact with the antenna element. The housing 8 is connected to a cable 11 that accommodates a switching signal to be applied to the switching circuit, a necessary power source, etc., and a coaxial cable 12 that leads a signal obtained by combining the outputs of each of the antenna elements to the main body of the direction finder. There is.

また第3図は本発明の他の実施例の縦断面図
で、導体板1は自動車の屋根であるが、この屋根
に上蓋を絶縁体で形成した筐体13を吸盤あるい
は磁石14で固定してある。その筐体中に接地導
体板6と帯状アンテナ素子4,5および筐体8等
を設けて、垂直アンテナ素子10を筐体13の中
央部から上方へ突出させたものである。
FIG. 3 is a longitudinal cross-sectional view of another embodiment of the present invention, in which the conductor plate 1 is the roof of an automobile, and a housing 13 with a top cover made of an insulator is fixed to the roof with a suction cup or a magnet 14. There is. A ground conductor plate 6, band-shaped antenna elements 4 and 5, a housing 8, etc. are provided in the housing, and a vertical antenna element 10 is made to protrude upward from the center of the housing 13.

第4図は上記アンテナ素子4,5および10の
平面図、並びにこれらに接続された電子的切換回
路15,16と位相調整回路17および合成回路
18の構成を示した図で、合成回路18の出力が
前記同軸ケーブル12によつて受信機に導かれ
る。また切換回路15,16には、第1図あるい
は第3図のケーブル11によつて端子19,20
から第5図A,Bに示したように、アンテナ素子
4と5の交叉角に相当する90度の位相差をもつた
矩形切換信号が加えられ、垂直アンテナ素子10
の出力は切換スイツチ21を介して上記位相調整
回路17またはケーブル22で通信用送受信機に
接続される。すなわち上記信号Aが正の期間は第
6図のようにアンテナ素子4の下端が特性インピ
ーダンスに等しい抵抗23により接地されて上端
から出力が送出され、また負の期間は逆に上端が
接地されて下端から合成回路18に出力が加わ
る。更に信号Bが正の期間は第6図のようにアン
テナ素子5の右端が特性インピーダンスに等しい
抵抗24で接地されて左端から出力が送出され、
負の期間は逆に左端が接地されて右端から出力が
送出される。
FIG. 4 is a plan view of the antenna elements 4, 5, and 10, and a diagram showing the configurations of the electronic switching circuits 15, 16, the phase adjustment circuit 17, and the combining circuit 18 connected thereto. The output is conducted by the coaxial cable 12 to a receiver. Further, the switching circuits 15 and 16 are connected to terminals 19 and 20 by the cable 11 shown in FIG. 1 or 3.
As shown in FIGS. 5A and 5B, a rectangular switching signal with a phase difference of 90 degrees corresponding to the intersecting angle of antenna elements 4 and 5 is applied, and vertical antenna element 10
The output is connected via the changeover switch 21 to the phase adjustment circuit 17 or the communication transmitter/receiver via the cable 22. That is, when the signal A is positive, the lower end of the antenna element 4 is grounded by the resistor 23 equal to the characteristic impedance and the output is sent from the upper end, as shown in FIG. 6, and when the signal A is negative, conversely, the upper end is grounded. The output is applied to the combining circuit 18 from the lower end. Furthermore, during the period when the signal B is positive, the right end of the antenna element 5 is grounded through a resistor 24 equal to the characteristic impedance, and the output is sent out from the left end, as shown in FIG.
Conversely, during the negative period, the left end is grounded and the output is sent from the right end.

第7図は第6図の状態におけるアンテナ素子
4,5の指向性を示したカージオイド曲線R,S
およびこれらの素子4,5の合成出力の指向性曲
線すなわち曲線R,Sを合成して得られるカージ
オイド曲線Tを示したものである。しかしつぎに
第5図における信号Aの極性が反転すると、第6
図に示したアンテナ素子4の上端が接地されて下
端から出力が送出される。従つて第7図における
曲線Rが原点Oに対して上下を反転した形状とな
り、このため合成曲線Tがこれを90度左回転した
状態となる。すなわち第5図の期間a,b,c,
dにおいてアンテナ素子4,5の合成指向性は第
8図にカージオイド曲線T,U,V,Wで示した
ように90度間隔をもつて間歇的に回転する。この
ため矢印zで示した方向から電波が入射したもの
とすると、上記期間a,b,c,dにおける帯状
アンテナ素子4および5の合成出力はそれぞれO
−t,O−u,O−v,O−wと変化する。第9
図Cはこの場合における素子4,5の合成出力で
ある。
FIG. 7 shows cardioid curves R and S showing the directivity of the antenna elements 4 and 5 in the state shown in FIG.
2 shows a directivity curve of the combined output of these elements 4 and 5, that is, a cardioid curve T obtained by combining curves R and S. However, when the polarity of signal A in FIG. 5 is reversed,
The upper end of the antenna element 4 shown in the figure is grounded, and the output is sent out from the lower end. Therefore, the curve R in FIG. 7 has a shape that is upside down with respect to the origin O, and therefore the composite curve T has a shape that is rotated 90 degrees to the left. That is, periods a, b, c in Fig. 5,
At d, the combined directivity of the antenna elements 4 and 5 rotates intermittently at 90 degree intervals as shown by cardioid curves T, U, V, and W in FIG. Therefore, assuming that radio waves are incident from the direction indicated by arrow z, the combined output of the band-shaped antenna elements 4 and 5 during the above periods a, b, c, and d is respectively O.
-t, O-u, O-v, O-w. 9th
Figure C shows the combined output of elements 4 and 5 in this case.

また垂直アンテナ素子10は無指向性であるか
らその出力は第9図Dに示したように電波の入射
方向および時間に関係なく一定の振幅を保持す
る。従つて第4図のスイツチ21を図の状態にし
ておくと、この出力が位相調整回路17を介して
合成回路18で前記第9図Cのような帯状アンテ
ナ素子4,5の合成出力に加えられる。このた
め、位相調整回路17により垂直アンテナ素子1
0の出力の位相を帯状アンテナ素子4,5の出力
と同相にすると、合成回路18の出力は第9図E
のようになる。この合成出力を同軸ケーブル12
で受信回路に導いて振幅検波を行うと、第9図F
のように同図Cのりんかく線に相当する低周波信
号が得られる。従つてこの信号を例えば狭帯域の
瀘波器に加えて第5図の矩形波と同一周波数の正
弦波成分を抽出し、その位相を検出することによ
つて第8図における矢印zのような電波の入射方
向を検出することができる。すなわちこの場合は
垂直アンテナ素子10の出力を帯状アンテナ素子
4,5の出力に同相で合成してあるから、第9図
Eのように振幅が増大して、このため特に電波が
微弱な場合に高周波雑音成分の影響が除去されて
正確な方位検出を行い得る。
Further, since the vertical antenna element 10 is non-directional, its output maintains a constant amplitude regardless of the incident direction and time of the radio waves, as shown in FIG. 9D. Therefore, if the switch 21 in FIG. 4 is kept in the state shown in the figure, this output is sent via the phase adjustment circuit 17 to the combining circuit 18 in addition to the combined output of the band-shaped antenna elements 4 and 5 as shown in FIG. 9C. It will be done. For this reason, the vertical antenna element 1 is controlled by the phase adjustment circuit 17.
When the phase of the output of 0 is made the same phase as the output of the strip antenna elements 4 and 5, the output of the combining circuit 18 is as shown in FIG.
become that way. This composite output is connected to the coaxial cable 12
When the signal is guided to the receiving circuit and amplitude detection is performed, Fig. 9
A low frequency signal corresponding to the link line C in the figure is obtained as shown in FIG. Therefore, by applying this signal to, for example, a narrow band filter, extracting a sine wave component having the same frequency as the rectangular wave in FIG. The direction of incidence of radio waves can be detected. In other words, in this case, since the output of the vertical antenna element 10 is combined with the outputs of the strip antenna elements 4 and 5 in the same phase, the amplitude increases as shown in FIG. The influence of high frequency noise components is removed and accurate direction detection can be performed.

また第4図、第6図に示した位相調整回路17
により垂直アンテナ素子10の出力を約90度移相
させて、帯状アンテナ素子4,5の合成出力との
間に90度の位相差を与えると、合成回路18の出
力の位相が第9図Cに示したような帯状アンテナ
素子4,5の合成出力の振幅に応じて変化する。
従つて受信回路においては、ケーブル12の出力
を振幅制限器に加えて一定の振幅となしたのち例
えば周波数弁別器に加えるときは第9図Gのよう
なパルス信号を得ることができる。その信号を前
述のように狭帯域瀘波器に加えて第5図の矩形波
と同一周波数の正弦波成分を抽出すると、この信
号の位相によつて電波の到来方向が指示される。
すなわち電波の到来方向に関係なく一定の振幅の
出力を得ることのできる垂直アンテナ素子10を
設け、その出力を移相して帯状アンテナ素子の出
力に合成することにより、位相または周波数変調
波を得るときは電波の断続によつて増幅器の自動
利得制御回路が機能しないような場合でも正確な
方位測定を行い得る作用効果が得られる。
In addition, the phase adjustment circuit 17 shown in FIGS. 4 and 6
When the output of the vertical antenna element 10 is phase-shifted by about 90 degrees and a phase difference of 90 degrees is given between the output of the vertical antenna element 10 and the composite output of the strip antenna elements 4 and 5, the phase of the output of the composite circuit 18 becomes as shown in FIG. It changes depending on the amplitude of the combined output of the band-shaped antenna elements 4 and 5 as shown in FIG.
Therefore, in the receiving circuit, when the output of the cable 12 is applied to an amplitude limiter to have a constant amplitude and then applied to, for example, a frequency discriminator, a pulse signal as shown in FIG. 9G can be obtained. When this signal is applied to a narrowband filter as described above to extract a sine wave component having the same frequency as the rectangular wave shown in FIG. 5, the direction of arrival of the radio wave is indicated by the phase of this signal.
That is, by providing a vertical antenna element 10 that can obtain an output with a constant amplitude regardless of the direction in which radio waves arrive, and by shifting the phase of the output and combining it with the output of the strip antenna element, a phase or frequency modulated wave is obtained. Even when the automatic gain control circuit of the amplifier does not function due to intermittent radio waves, it is possible to obtain accurate azimuth measurements.

なお以上は互に直交するように配置した2つの
帯状アンテナ素子を用いた場合について説明した
が、このような装置はアンテナ素子の長さと電波
の波長との関係によつて8分円誤差を生ずる。し
かし例えば4個のアンテナ素子を45度間隔で配置
するときは8分円誤差が消滅して比較的小さい16
分円誤差だけが残るから、更に広い周波数範囲に
亘つて高精度の方位測定を行うことができる。
Although the above explanation uses two band-shaped antenna elements arranged perpendicular to each other, such a device produces an octant error due to the relationship between the length of the antenna element and the wavelength of the radio wave. . However, for example, when four antenna elements are arranged at 45 degree intervals, the octant circle error disappears and becomes relatively small16
Since only the circular error remains, highly accurate azimuth measurement can be performed over a wider frequency range.

また通信用送受信機のアンテナは受信周波数に
同調していることが多いために、方向探知電波の
周波数が通信に用いられる周波数帯と同じである
と、干渉によつて方向探知に大きな誤差を与え
る。このような場合に前記第4図のケーブル22
を通信用送受信機に接続して、垂直アンテナ素子
10を共用することにより、上述の難点が除去さ
れる。なおこのような場合に通信用受信回路はこ
れを方向探知機の増幅部として利用することがで
きる。
Additionally, since the antennas of communication transmitters and receivers are often tuned to the receiving frequency, if the frequency of direction-finding radio waves is the same as the frequency band used for communication, interference will cause large errors in direction-finding. . In such a case, the cable 22 shown in FIG.
By connecting the vertical antenna elements 10 to a communication transceiver and sharing the vertical antenna element 10, the above-mentioned difficulties are eliminated. Note that in such a case, the communication receiving circuit can be used as an amplifier section of the direction finder.

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

第1図は本発明実施例の縦断面図、第2図は第
1図の一部を截欠した平面図、第3図は本発明の
他の実施例の縦断面図、第4図は本発明実施例の
電気的構成を示した図、第5図は第4図における
帯状アンテナ素子の切換信号波形図、第6図はア
ンテナ素子の一切換状態における第4図の装置の
回路を示した図、第7図は第6図の状態における
帯状アンテナ素子の指向特性曲線、第8図はアン
テナ素子の各切換状態における指向特性曲線、第
9図は本発明実施例の動作を説明する波形図であ
る。なお図において、1は導体板、2は円孔、3
は絶縁体板、4,5は帯状アンテナ素子、6は導
体板、7は隆起部、8は筐体、9は同軸ケーブ
ル、10は垂直アンテナ素子、11はケーブル、
12は同軸ケーブル、15,16は切換回路、1
7は位相調整回路、18は合成回路である。
FIG. 1 is a longitudinal sectional view of an embodiment of the present invention, FIG. 2 is a partially cutaway plan view of FIG. 1, FIG. 3 is a longitudinal sectional view of another embodiment of the invention, and FIG. A diagram showing the electrical configuration of an embodiment of the present invention, FIG. 5 is a switching signal waveform diagram of the strip antenna element in FIG. 4, and FIG. 6 shows a circuit of the device in FIG. 7 is a directional characteristic curve of the strip antenna element in the state shown in FIG. 6, FIG. 8 is a directional characteristic curve in each switching state of the antenna element, and FIG. 9 is a waveform explaining the operation of the embodiment of the present invention. It is a diagram. In the figure, 1 is a conductor plate, 2 is a circular hole, and 3 is a conductor plate.
is an insulator plate, 4 and 5 are strip antenna elements, 6 is a conductor plate, 7 is a raised portion, 8 is a housing, 9 is a coaxial cable, 10 is a vertical antenna element, 11 is a cable,
12 is a coaxial cable, 15 and 16 are switching circuits, 1
7 is a phase adjustment circuit, and 18 is a synthesis circuit.

Claims (1)

【特許請求の範囲】[Claims] 1 実質的に接地された導体板の上に複数個の帯
状アンテナ素子をそれらの中央部が互に絶縁され
て交叉するように適当な距離を介して重合し各ア
ンテナ素子の両端をそれらの交叉角に相当する位
相差をもつて一定の周期で交互に接地して他端か
ら受信出力を送出する複数個の電子的切換回路
と、前記帯状アンテナ素子の中央部に配置した垂
直アンテナ素子と、上記電子的切換回路の各々の
出力および垂直アンテナ素子の出力を適宜の位相
関係で合成する回路とよりなることを特徴とする
方向探知機の空中線装置
1 A plurality of strip antenna elements are superimposed on a substantially grounded conductive plate at an appropriate distance so that their central portions are insulated and intersect with each other, and both ends of each antenna element are a plurality of electronic switching circuits that are alternately grounded at a constant period with a phase difference corresponding to the angle and transmit the received output from the other end; and a vertical antenna element disposed in the center of the strip antenna element; An antenna device for a direction finder, comprising a circuit that combines the outputs of each of the electronic switching circuits and the output of the vertical antenna element in an appropriate phase relationship.
JP13014184A 1984-06-26 1984-06-26 Antenna system of direction finder Granted JPS6110302A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13014184A JPS6110302A (en) 1984-06-26 1984-06-26 Antenna system of direction finder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13014184A JPS6110302A (en) 1984-06-26 1984-06-26 Antenna system of direction finder

Publications (2)

Publication Number Publication Date
JPS6110302A JPS6110302A (en) 1986-01-17
JPH0449803B2 true JPH0449803B2 (en) 1992-08-12

Family

ID=15026943

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13014184A Granted JPS6110302A (en) 1984-06-26 1984-06-26 Antenna system of direction finder

Country Status (1)

Country Link
JP (1) JPS6110302A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5300936A (en) * 1992-09-30 1994-04-05 Loral Aerospace Corp. Multiple band antenna
JP4839118B2 (en) * 2006-03-30 2011-12-21 積水化学工業株式会社 Synthetic sleepers for linear railway

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60377A (en) * 1983-06-17 1985-01-05 Taiyo Musen Kk Antenna device of direction detector

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60377A (en) * 1983-06-17 1985-01-05 Taiyo Musen Kk Antenna device of direction detector

Also Published As

Publication number Publication date
JPS6110302A (en) 1986-01-17

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