JPS6339877B2 - - Google Patents
Info
- Publication number
- JPS6339877B2 JPS6339877B2 JP7915882A JP7915882A JPS6339877B2 JP S6339877 B2 JPS6339877 B2 JP S6339877B2 JP 7915882 A JP7915882 A JP 7915882A JP 7915882 A JP7915882 A JP 7915882A JP S6339877 B2 JPS6339877 B2 JP S6339877B2
- Authority
- JP
- Japan
- Prior art keywords
- output
- circuit
- phase
- signal
- sense
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/02—Direction-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
- G01S3/14—Systems for determining direction or deviation from predetermined direction
- G01S3/58—Rotating 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
- G01S3/60—Broad-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
- G01S3/64—Broad-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 wherein the phase angle of the signal is determined by phase comparison with a reference alternating signal varying in synchronism with the directivity variation
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Description
方向探知機を船舶等に設置する場合は、その空
中線の近傍にマストあるいはステー等の電波に擾
乱を与える物が多数存在することを避け得ない。
特にセンス決定用の垂直空中線は、高周波的接地
点が不安定になるためにマスト、ステー等の影響
が大きく、出力の振幅並びに位相が電波の到来方
向によつて著しく変動し、センスが不鮮明になる
ことが多い。本発明はこのような欠点を除去し、
常に明確なセンスを行つて、電波の到来方向を正
確に測定しようとするものである。
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1対の枠型
空中線1,2の出力を平衡変調器3,4に加え
て、例えば135Hgの低周波発振器5から送出され
る互に90度の位相差を有する信号a,bで変調す
ると共に極性制御器6,7に加えて信号発生器8
の出力で無線周波の極性を制御してある。また無
指向性の垂直空中線9とその出力を加えられる90
度位相器10とよりなる第1センス回路を設けて
その出力をスイツチ回路11に加え、このスイツ
チ回路の出力並びに前記変調器3,4および極性
制御器6,7の出力を合成回路12に加えてあ
る。その合成回路12の出力を無線受信回路13
に加えて増幅検波することにより前記135Hgの低
周波信号を復調し、上記周波数の狭帯域フイルタ
14を介してレベル検出器15および位相検出回
路16に加えてある。レベル検出器15はフイル
タ14の出力が所定のレベルを越すと例えば0.5
秒程度の微小の時間遅れをもつて信号を送出する
から、この信号で前記スイツチ回路11が開放
し、かつ信号発生器8が起動する。また位相検出
回路16には発振器5から適当な一定位相の低周
波信号が位相基準として加えられている。その出
力信号がブラウン管あるいはデジタル位相計のよ
うな表示器17に加えられて電波の到来方向を指
示すると共に上記出力信号は信号発生器8にも加
わる。
この装置において、レベル検出器15が信号を
送出していない状態ではスイツチ回路11が閉成
し、また信号発生器8は制御器6,7に枠型空中
線1,2の出力を遮断する信号「0」を加えてい
る。装置を起動すると枠型空中線1,2の出力が
平衡変調器3,4において互に90度の位相差を有
する信号a,bでそれぞれ変調され、、また垂直
空中線9等の第1センス回路の出力はスイツチ回
路11を介して、合成回路12に加わる。その合
成信号が受信回路13に加わつて、発振器5の出
力低周波成分が復調され、狭帯域フイルタ14に
よつて雑音成分が完全に除去される。従つて位相
検出回路16でフイルタ14の出力信号の位相を
検出することにより、位相表示器17で電波の到
来方向を表示することができる(特開昭55−
124079号)。
かつ上述の動作が完全に行われる程度の電波が
空中線1,2および9に入射しているものとする
とフイルタ14から充分大きい出力信号が送出さ
れるから、レベル検出器15が前述のように微小
の時間遅れをもつて信号を送出し、この信号でス
イツチ回路11が開放して第1センス回路の出力
が遮断される。また検出器15の出力が信号発生
器8に加わると、位相検出回路16の出力信号、
従つて電波の到来方向に応じて該発生器8から極
性制御器6,7の次表のような信号が加わり、該
制御器は信号「1」
When installing a direction finder on a ship or the like, it is unavoidable that there are many objects near the antenna that disturb radio waves, such as masts or stays.
In particular, vertical antennas used to determine sense are highly influenced by masts, stays, etc. because the high-frequency grounding point becomes unstable, and the amplitude and phase of the output fluctuate significantly depending on the direction of arrival of radio waves, making the sense unclear. It often happens. The present invention eliminates such drawbacks and
It is an attempt to accurately measure the direction of arrival of radio waves by always performing a clear sense. FIG. 1 is a diagram showing the configuration of an embodiment of the present invention, in which the outputs of a pair of frame-shaped antennas 1 and 2 arranged so that their directivities are orthogonal to each other are applied to balanced modulators 3 and 4. For example, it is modulated with signals a and b having a phase difference of 90 degrees, which are sent out from a low frequency oscillator 5 of 135 Hg, and in addition to polarity controllers 6 and 7, a signal generator 8
The polarity of the radio frequency is controlled by the output. In addition, an omnidirectional vertical antenna 9 and its output can be added 90
A first sense circuit consisting of a degree phase shifter 10 is provided and its output is applied to a switch circuit 11, and the output of this switch circuit and the outputs of the modulators 3, 4 and polarity controllers 6, 7 are applied to a synthesis circuit 12. There is. The output of the combining circuit 12 is sent to the radio receiving circuit 13.
In addition, the 135 Hg low frequency signal is demodulated by amplification and detection, and is applied to the level detector 15 and phase detection circuit 16 via the narrow band filter 14 of the above frequency. When the output of the filter 14 exceeds a predetermined level, the level detector 15 detects, for example, 0.5
Since the signal is sent out with a minute delay of about seconds, this signal opens the switch circuit 11 and activates the signal generator 8. Further, a low frequency signal of a suitable constant phase is applied from the oscillator 5 to the phase detection circuit 16 as a phase reference. The output signal is applied to a display 17 such as a cathode ray tube or a digital phase meter to indicate the arrival direction of the radio wave, and the output signal is also applied to a signal generator 8. In this device, when the level detector 15 is not sending out a signal, the switch circuit 11 is closed, and the signal generator 8 sends a signal to the controllers 6 and 7 to cut off the output of the frame antennas 1 and 2. 0" is added. When the device is started, the outputs of the frame antennas 1 and 2 are modulated by the signals a and b having a phase difference of 90 degrees in the balanced modulators 3 and 4, respectively, and the outputs of the first sense circuit of the vertical antenna 9, etc. The output is applied to a synthesis circuit 12 via a switch circuit 11. The synthesized signal is applied to the receiving circuit 13, and the output low frequency component of the oscillator 5 is demodulated, and the noise component is completely removed by the narrow band filter 14. Therefore, by detecting the phase of the output signal of the filter 14 with the phase detection circuit 16, the direction of arrival of the radio wave can be displayed on the phase indicator 17 (Japanese Patent Application Laid-Open No. 1983-1999).
No. 124079). Assuming that enough radio waves are incident on the antennas 1, 2, and 9 for the above-mentioned operation to be completed, a sufficiently large output signal will be sent out from the filter 14, so that the level detector 15 will detect a very small signal as described above. A signal is sent out with a time delay of , and this signal opens the switch circuit 11 and cuts off the output of the first sense circuit. Further, when the output of the detector 15 is applied to the signal generator 8, the output signal of the phase detection circuit 16,
Therefore, depending on the arrival direction of the radio wave, signals as shown in the following table are added from the generator 8 to the polarity controllers 6 and 7, and the controller outputs the signal "1".
【表】
を加えられると枠型空中線の出力極性を反転する
ことなく送出し、「−1」を加えられると極性を
反転して送出する。
枠型空中線1,2と極性制御器6,7等は第2
センス回路を形成している。その空中線1が第2
図のように電波の到来方向を示す角度90―270゜の
方向、空中線2が0―180゜の方向に配置されて、
矢印wのように電波の到来方向が0〜90゜の範囲
にある場合に該空中線1,2が共に正極性の出力
を送出するものとすると、この状態では極性制御
器6,7に前記表のように何れも信号「1」が加
わるから、上記空中線の出力は共に極性を反転す
ることなく送出される。またもし電波の到来方向
が90〜180゜の範囲になると空中線2の出力の極性
が反転する。しかし同時に制御器7に加わる信号
が「−1」になつて入力と逆の極性の出力が得ら
れる。更に電波の到来方向が180〜270゜の範囲に
なると空中線1,2の出力の極性が何れも逆位相
となるが、制御器6,7に加わる信号も共に「−
1」となり、270〜360゜の範囲になると空中線1
の出力のみが逆位相となるが同時に制御器6に加
わる信号のみが「−1」となつてその極性を反転
する。従つて制御器6,7は電波の到来方向に関
係なく、常に該電波が0〜90゜の範囲に到来した
場合と同一の極性の出力を送出する。
更に、第2図に矢印wで示した方向から線分0
―pで与えられる強度の電波が入射するものとす
ると、空中線1,2にはそれぞれ0―s,0―r
で示される出力が発生する。かつこれらの出力は
前述のように合成回路12において同位相で合成
されるから線分0―vで示される強度の入力とし
て受信回路13に加わる。また矢印wの方向を0
〜90゜の範囲で変化すると、点vが点0から45゜の
方向にある点qを中心として上記点0を通る円弧
Aで与えられる軌跡をもつて移動する。更に90〜
180゜、180〜270゜、270〜360゜の各角度で入射する
場合も同様にして円弧BあるいはC,D等の軌跡
をとり、かつその位相は入射角度が0〜90゜の場
合と同一である。
すなわち前述のようにレベル検出器15が信号
を送出して第1センス回路の出力が遮断される
と、枠型空中線1,2および制御器6,7等から
なる第2センス回路の出力が平衡変調器3,4の
出力と共に受信回路13に加わり、かつこの第2
センス回路の出力は第2図における4つの円弧
A,B,C,Dで示されるように強度がほぼ一定
で、しかも電波の入射方向に関係なく常に一定の
位相を有する。従つて受信回路13で復調された
出力信号の位相を検出回路16で検出して表示器
17で表示することにより電波の到来方向を知る
ことができる。
しかもこの場合は枠型空中線1,2によつてセ
ンス入力を得るから、変調器3,4の出力に対し
て確実に一定の位相と振幅とを有する。すなわち
垂直空中線の出力のように、近傍の擾乱物体の影
響で枠型空中線の出力と無関係に位相並びに振幅
の変動を生じないから、極めて正確な方位を安定
に測定することができる。なお測定の開始に際し
ては前述のようにまず第1センス回路の出力を利
用して制御器6,7による極性の切換えを行うか
らこの場合は上述のように方向の誤観測を生ずる
ことがある。その誤観測が0〜90゜、90〜180゜、
…の範囲内にある場合は勿論何等の支障をも生じ
ない。また電波の真の入射方向が第2図のように
0〜90゜の範囲における矢印xである場合にこれ
を矢印yのように90〜180゜の範囲内に誤観測を生
じたものとすると、矢印xが円弧Aと交わる点を
t、円弧Aを点tと逆の方向へほぼ等距離だけ延
長した点をuとするとき、第2センス回路の出力
が0―uで示される値になる。しかし矢印xとy
の間の角度、すなわち測定誤差は一般に比較的小
さい値であるから、出力0―uが著しく小さくな
つて第2センス回路による観測が不可能になるよ
うなおそれはないものである。しかも第2センス
回路によつて前述のように正確な観測が開始され
ると、このセンス回路の出力は正規の値0―tと
なるから、その後は正常な状態で動作する。
以上実施例について説明したように本発明は指
向性のある枠型空中線によつてセンス決定用の出
力を得ることができる。従つて垂直空中線による
センス決定出力のように実効的接地点の不安定あ
るいは近傍の擾乱物体による出力の著しい変動等
がなく、指向性出力に対して確実に一定の位相と
ほぼ一定の割合の封幅とをもつたセンス出力が得
られて、このため正確な測定を安定に行うことが
できる作用効果が得られる。[Table] When ``-1'' is added, the output polarity of the frame antenna is sent out without being inverted, and when ``-1'' is added, the polarity is inverted and sent out. Frame type antennas 1, 2 and polarity controllers 6, 7, etc. are the second
Forms a sense circuit. The antenna 1 is the second
As shown in the figure, the antenna 2 is placed in the direction of an angle of 90-270° indicating the direction of arrival of radio waves, and the antenna 2 is placed in the direction of 0-180°.
Assuming that both the antennas 1 and 2 send out outputs of positive polarity when the arrival direction of the radio waves is in the range of 0 to 90 degrees as shown by arrow w, in this state, the polarity controllers 6 and 7 Since the signal "1" is applied to both of them, the outputs of the above antennas are transmitted without reversing the polarity. Furthermore, if the direction of arrival of radio waves falls within the range of 90 to 180 degrees, the polarity of the output of the antenna 2 will be reversed. However, at the same time, the signal applied to the controller 7 becomes "-1" and an output having the opposite polarity to the input is obtained. Furthermore, when the direction of arrival of the radio wave is in the range of 180 to 270 degrees, the polarities of the outputs of the antennas 1 and 2 will both be in opposite phase, but the signals applied to the controllers 6 and 7 will also be "-".
1", and when the angle is between 270 and 360 degrees, the antenna becomes 1.
Only the output of the controller 6 has an opposite phase, but at the same time only the signal applied to the controller 6 becomes "-1" and its polarity is reversed. Therefore, the controllers 6 and 7 always send outputs with the same polarity as when the radio waves arrive in the range of 0 to 90 degrees, regardless of the direction in which the radio waves arrive. Furthermore, from the direction shown by arrow w in Fig. 2, line segment 0
- Assuming that a radio wave with an intensity given by p is incident, antennas 1 and 2 have 0-s and 0-r, respectively.
The output shown is generated. Since these outputs are combined in the same phase in the combining circuit 12 as described above, they are applied to the receiving circuit 13 as an input with the intensity shown by the line segment 0-v. Also, change the direction of arrow w to 0
When the angle changes within the range of ~90 degrees, point v moves with a trajectory given by arc A passing through point 0, centering on point q in the direction of 45 degrees from point 0. 90 more
Similarly, when the incident angle is 180°, 180~270°, or 270~360°, the locus of arc B, C, D, etc. is taken, and the phase is the same as when the incident angle is 0~90°. It is. That is, when the level detector 15 sends a signal and the output of the first sense circuit is cut off as described above, the output of the second sense circuit consisting of the frame antennas 1, 2, controllers 6, 7, etc. becomes balanced. It is applied to the receiving circuit 13 along with the outputs of the modulators 3 and 4, and
The output of the sense circuit has approximately constant intensity as shown by the four arcs A, B, C, and D in FIG. 2, and also always has a constant phase regardless of the direction of incidence of the radio waves. Therefore, by detecting the phase of the output signal demodulated by the receiving circuit 13 by the detecting circuit 16 and displaying it on the display 17, it is possible to know the direction of arrival of the radio wave. Moreover, in this case, since the sense input is obtained by the frame antennas 1 and 2, it is ensured that the outputs of the modulators 3 and 4 have a constant phase and amplitude. That is, unlike the output of a vertical antenna, fluctuations in phase and amplitude do not occur regardless of the output of a frame-shaped antenna due to the influence of nearby disturbing objects, so extremely accurate azimuth can be stably measured. Note that when starting the measurement, as described above, the output of the first sense circuit is first used to switch the polarity by the controllers 6 and 7, so in this case, erroneous observation of the direction may occur as described above. The erroneous observation is 0 to 90°, 90 to 180°,
Of course, if it is within the range of ..., no problem will occur. In addition, if the true incident direction of the radio wave is arrow x in the range of 0 to 90 degrees as shown in Figure 2, if we assume that this is erroneously observed in the range of 90 to 180 degrees as shown in arrow y. , when the point where the arrow x intersects with the arc A is t, and the point where the arc A is extended by approximately the same distance in the opposite direction to the point t is u, the output of the second sense circuit is a value indicated by 0-u. Become. But arrows x and y
Since the angle between them, that is, the measurement error, is generally a relatively small value, there is no risk that the outputs 0-u will become so small that they will become impossible to observe by the second sense circuit. Furthermore, once accurate observation is started by the second sense circuit as described above, the output of this sense circuit becomes the normal value 0-t, so that the second sense circuit operates in a normal state thereafter. As described above with respect to the embodiments, the present invention can obtain an output for sense determination using a directional frame-shaped antenna. Therefore, unlike the sense decision output from a vertical antenna, there is no instability in the effective grounding point or significant fluctuations in the output due to nearby disturbing objects, and the directional output can be reliably kept at a constant phase and a nearly constant rate of sealing. A sense output having a certain width can be obtained, and therefore, an effect that accurate measurement can be stably performed can be obtained.
第1図は本発明実施例の構成を示した図、第2
図は本発明の原理を説明する線図である。なお図
において、1,2は枠型空中線、3,4は平衡変
調器、5は低周波発振器、6,7は極性制御器、
8は信号発生器、9は垂直空中線、10は90度移
相器、11はスイツチ回路、12は合成回路、1
3は受信回路、14はフイルタ、15はレベル検
出器、16は位相検出回路、17は表示器であ
る。
Figure 1 is a diagram showing the configuration of an embodiment of the present invention, Figure 2 is a diagram showing the configuration of an embodiment of the present invention.
The figure is a diagram explaining the principle of the present invention. In the figure, 1 and 2 are frame antennas, 3 and 4 are balanced modulators, 5 is a low frequency oscillator, 6 and 7 are polarity controllers,
8 is a signal generator, 9 is a vertical antenna, 10 is a 90 degree phase shifter, 11 is a switch circuit, 12 is a synthesis circuit, 1
3 is a receiving circuit, 14 is a filter, 15 is a level detector, 16 is a phase detection circuit, and 17 is a display.
Claims (1)
の枠型空中線と、垂直空中線の出力を90度移相さ
せる第1センス回路と、90度の位相差を有する2
つの低周波信号を送出する発振器と、前記1対の
枠型空中線の各々の出力を上記2つの低周波信号
の各々でそれぞれ変調する1対の変調器と、上記
第1センス回路および1対の変調器の合成出力を
入力とし前記発振器の出力と同一周波数の信号を
復調する受信回路と、上記受信回路の復調出力の
位相を検出する位相検出回路と、上記位相検出回
路の出力信号によつて電波の到来方向を指示する
表示器とよりなり、更に上記位相検出回路の出力
信号に応じて前記1対の枠型空中線の出力をそれ
ぞれ適宜の極性で合成することにより電波到来方
向に関係なく一定の位相とほぼ一定の振幅とを有
する信号を得る第2センス回路と、前記第1セン
ス回路から受信回路に加えられる入力を必要に応
じて上記第2センス回路の出力に切換える回路と
を設けたことを特徴とする方向探知機。1 A pair of frame-shaped antennas arranged so that the directivity is orthogonal to each other, a first sense circuit that shifts the output of the vertical antenna by 90 degrees, and 2 having a phase difference of 90 degrees.
an oscillator that sends out two low frequency signals; a pair of modulators that modulate the outputs of each of the pair of frame antennas with each of the two low frequency signals; a receiving circuit that receives the combined output of the modulator and demodulates a signal having the same frequency as the output of the oscillator; a phase detection circuit that detects the phase of the demodulated output of the receiving circuit; and an output signal of the phase detection circuit. It consists of an indicator that indicates the direction in which the radio waves arrive, and furthermore, the outputs of the pair of frame-shaped antennas are combined with appropriate polarity according to the output signal of the phase detection circuit, so that the polarity remains constant regardless of the direction in which the radio waves arrive. a second sense circuit that obtains a signal having a phase and a substantially constant amplitude, and a circuit that switches the input applied from the first sense circuit to the receiving circuit to the output of the second sense circuit as necessary. A direction finder characterized by:
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7915882A JPS58196473A (en) | 1982-05-13 | 1982-05-13 | Direction finder |
| KR8205655A KR870000138B1 (en) | 1982-04-05 | 1982-12-17 | Auto direction finder |
| DE3248324A DE3248324C2 (en) | 1982-04-05 | 1982-12-28 | Automatic radio compass |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7915882A JPS58196473A (en) | 1982-05-13 | 1982-05-13 | Direction finder |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS58196473A JPS58196473A (en) | 1983-11-15 |
| JPS6339877B2 true JPS6339877B2 (en) | 1988-08-08 |
Family
ID=13682144
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7915882A Granted JPS58196473A (en) | 1982-04-05 | 1982-05-13 | Direction finder |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58196473A (en) |
-
1982
- 1982-05-13 JP JP7915882A patent/JPS58196473A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS58196473A (en) | 1983-11-15 |
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