JPS60103A - Beam width variable antenna - Google Patents

Beam width variable antenna

Info

Publication number
JPS60103A
JPS60103A JP10716583A JP10716583A JPS60103A JP S60103 A JPS60103 A JP S60103A JP 10716583 A JP10716583 A JP 10716583A JP 10716583 A JP10716583 A JP 10716583A JP S60103 A JPS60103 A JP S60103A
Authority
JP
Japan
Prior art keywords
sub
reflector
antenna
reception level
beam width
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.)
Pending
Application number
JP10716583A
Other languages
Japanese (ja)
Inventor
Noriyasu Toyonaga
豊永 憲康
Kiyoharu Murayama
村山 清春
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.)
Fujitsu Ltd
Original Assignee
Fujitsu 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 Fujitsu Ltd filed Critical Fujitsu Ltd
Priority to JP10716583A priority Critical patent/JPS60103A/en
Publication of JPS60103A publication Critical patent/JPS60103A/en
Pending legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00Antennas or antenna systems providing at least two radiating patterns
    • H01Q25/002Antennas or antenna systems providing at least two radiating patterns providing at least two patterns of different beamwidth; Variable beamwidth antennas

Landscapes

  • Radio Transmission System (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 (a) 発明の技術分野 本発明はビーム巾可変空中線に係シ、特にダクト性フェ
ージングの発生する無線通信回線に使用するビーム中可
変空中線に関するものである。
DETAILED DESCRIPTION OF THE INVENTION (a) Technical Field of the Invention The present invention relates to a variable beam width antenna, and more particularly to a variable beam width antenna used in a wireless communication line where duct fading occurs.

(b) 従来技術と問題 マイクロ波を使用する多重無線装置が広く使用されてい
るが、伝播距離が長い場合や、海上伝播の場合、その低
電波の通る大気などの状況によってフェージングが発生
することがある。
(b) Conventional technology and problems Multiplex radio equipment using microwaves is widely used, but fading can occur when the propagation distance is long, when propagating over sea, and depending on the atmosphere through which the low radio waves pass. There is.

フェージングの主な種類は大気の屈折率の分布が変化す
るために、電波の伝播径路が曲げられて発生するダクト
性フェージングや、同時に受信された直接波と反射波の
位相状態によって2つの波が互に打ち消し合ったり又は
加え合ったシすることにより生ずるものなどがある。
The main types of fading are duct-induced fading, which occurs when the propagation path of radio waves is bent due to changes in the refractive index distribution of the atmosphere, and duct fading, which occurs when two waves are split due to the phase state of the direct wave and reflected wave received at the same time. There are some that are caused by canceling each other out or adding to each other.

ダクト性フェージングに対する対策としてスペース−ダ
イパーシティ方式、周波数・ダイパーシティ方式、送信
電力を増加する方式等がある。しかし乍ら上記スペース
・ダイパーシティ方式では2系統の空中線及び受信機が
必要であり、周波数ダイバシティ方式では2系統の送受
48機を用意しなければならない。又、送信電力増加の
場合には高出力電力増巾器が必要となる。
Measures against duct fading include a space-diaperity method, a frequency-diaperity method, and a method of increasing transmission power. However, the space diversity method requires two systems of antennas and receivers, and the frequency diversity method requires two systems of 48 transmitters and receivers. Furthermore, in the case of an increase in transmission power, a high output power amplifier is required.

即ち、空中線、送受信機が余分に必要で更にこれらの機
器と従来の機器と並列又は切替動作させなければならな
いので構成が複雑になるため価格も高価になるという問
題があった。
That is, an antenna and a transmitter/receiver are additionally required, and these devices and conventional devices must be operated in parallel or in a switched manner, resulting in a complicated configuration and an increase in price.

(c)発明の目的 本発明は上記従来技術の問題に鑑みなされたものであっ
て、ダクト性フェージングの発生によって生ずる影響を
軽減するだめのビーム巾可変空中線を提供することを目
的としている。
(c) Purpose of the Invention The present invention has been made in view of the problems of the prior art described above, and it is an object of the present invention to provide a variable beam width antenna that reduces the effects caused by the occurrence of duct fading.

(d) 発明の構成 上記発明の目的は主反射鏡、副反射鏡、1次放射器など
から構成された空中線に於て、′該空中線で受信した受
信レベルが一定時間継続して定められた値以下になって
いることを検知する手段と、該検知手段からの出力で複
数の副反射鏡支柱により固定された円板上に設置された
副反射鏡駆動部を制御する手段と、制御された該副反射
鏡駆動部により該副反射鏡を平行移動する手段とからな
ることを特徴とするビーム巾可変空中線ヲ提供すること
によυ達成される。
(d) Structure of the Invention The object of the above invention is to provide an antenna that is composed of a main reflector, a sub-reflector, a primary radiator, etc., and that the reception level received by the antenna is determined continuously for a certain period of time. a means for detecting that the value is below a value, a means for controlling a sub-reflector drive section installed on a disk fixed by a plurality of sub-reflector supports using the output from the detecting means; This is accomplished by providing a variable beam width antenna characterized by comprising means for moving the sub-reflector in parallel by the sub-reflector drive section.

(e) 発明の実施例 第1図は本発明の一実施例を説明するための図である。(e) Examples of the invention FIG. 1 is a diagram for explaining one embodiment of the present invention.

図中、1は主反射鏡面、2I′i1次放射器、3け副反
射鏡取付支柱、31は円板、32は補強部材、33は支
柱、4は副反射鏡、41は副反射鏡柱、42は副反射鏡
平面、43は副反射鏡支柱、5けモータ、6はクランク
機構部、7はフィーダー、RXは受信部、P/Nは受信
レベル検出器、OUTは出力端子をそれぞれ示す。
In the figure, 1 is the main reflecting mirror surface, 2I'i primary radiator, 3 sub-reflector mounting columns, 31 is a disk, 32 is a reinforcing member, 33 is a column, 4 is a sub-reflector, 41 is a sub-reflector column , 42 is a sub-reflector plane, 43 is a sub-reflector column, 5 motors, 6 is a crank mechanism, 7 is a feeder, RX is a receiver, P/N is a reception level detector, and OUT is an output terminal. .

そしてこれら各部は次のように接続されている。These parts are connected as follows.

同じ長さを有する例えば3本の副反射鏡取付支柱3の一
端が、回転放物面の形状を有する主反射鏡面上の3ケ所
(この回転放物面の回転軸を中心とした同一円周上にあ
り且つこの内周を3等分した点)に、他端が共通の円板
31の端にそれぞれ固着されている。そしてこの日板3
1の主反射鏡゛面イ則にこの円板と円心で且つこの同心
円の円周を3等分した点に中空の支柱33をそれぞれ鋲
などで固定する。この支柱33は補強のため副反射鏡駆
動部」支柱3と補強部材32で固着されている。
For example, one end of three sub-reflector mounting struts 3 having the same length are attached at three locations on the main reflecting mirror surface having the shape of a paraboloid of revolution (at the same circumference around the axis of rotation of this paraboloid of revolution). The other end is fixed to the end of a common disk 31, respectively, at the points located above and dividing this inner periphery into three equal parts. And this day board 3
Hollow pillars 33 are fixed with rivets or the like at the center of this disk and at points dividing the circumference of this concentric circle into three equal parts according to the plane of the main reflecting mirror 1. This support 33 is fixed to the support 3 of the sub-reflector driving section by a reinforcing member 32 for reinforcement.

又回転双曲面を回転軸に垂直な平面で切シ取った形状の
副反射鏡4の回転双曲面の部分は主反射鏡面1と相対し
、垂直な平面である副反射鏡平面42に垂直に3本の副
反射鏡柱41が固着されている。この副反射鏡柱41は
それぞれ対応する前記支柱33の中空部内を移動可能に
嵌合されている。そして更に副反射鏡平面42の中心部
に垂直に固着された副反射鏡支柱43は回転運動を直線
運動に変換する例えばクランク機構部6を介してモータ
5の回転軸と接続されている。
In addition, the hyperboloid of revolution part of the sub-reflector 4, which is shaped by cutting out the hyperboloid of revolution with a plane perpendicular to the rotation axis, faces the main reflector surface 1 and is perpendicular to the sub-reflector plane 42, which is a perpendicular plane. Three sub-reflector columns 41 are fixed. The sub-reflecting mirror columns 41 are movably fitted in the hollow portions of the corresponding columns 33, respectively. Further, a sub-reflector support column 43 fixed perpendicularly to the center of the sub-reflector plane 42 is connected to the rotating shaft of the motor 5 via, for example, a crank mechanism 6 that converts rotational motion into linear motion.

次に仁の主反射鏡面の中心の穴に固着された、円錐形を
成る高で底面と平行な面で切シ尖端部を取除いた形の開
口部の底面部を副反射鏡4と相対させ、ζり断さノまた
部分はフィーダを介して受信部RXの入力端子と接続さ
れ、この受信部RXの第1の出力端子は外部取出端子O
UTと、第2の出力端子は受信レベル検出器P/Nを介
して前記モータ5の入力端子にそれぞれ接続されている
Next, the bottom surface of the conical opening, which is fixed in the center hole of the main reflecting mirror surface and has the pointed end removed on a plane parallel to the bottom surface, is aligned with the sub-reflecting mirror 4. The ζ-cut portion is connected to the input terminal of the receiving section RX via a feeder, and the first output terminal of this receiving section RX is connected to the external output terminal O.
UT and the second output terminal are respectively connected to the input terminal of the motor 5 via a reception level detector P/N.

このように接続されている各部の動作は次のようである
The operations of each part connected in this way are as follows.

先ず正常な受信状態の場合は第1図に示した空中線の2
つの鏡面の位置は、主反射鏡1の焦点を02とし1次放
射器の放射特性によってきまる等価焦点をO7としたと
き副反射鏡1−1この2つの焦点OI及び02を共快焦
点とする回転双曲面となっている。この場合主反射鏡1
から放射される電波は平行状態で外部に放射される。逆
に子育状態で受信された電波■は主反射@1及び副反射
鏡゛4でそれぞれ反射され02点で焦点を結ぶ。そして
集められた電波はフィーダ7を通って受信部RXに加え
られこ\で増巾9周波数変換、復調され取り出された復
調波は端子1から外部に取り出されるが、伝送されるべ
き信号周波数帯域より例えば上の周波数帯に含まれる雑
音成分及びパイロット信号は受信レベル検出器P/Nに
加えられる。こ\で雑計成分及びパイロット信号のレベ
ルを検出し定めらノtだ受信レベル(標準受信レベルよ
り例えばadb下のレベル)に対応する雑音成分及びパ
イロット信号のレベルと比較し受信レベルを定められた
受信レベルよシも高いレベルの場合はこの受信レベル検
出器P/Nの出力は0でモータ5は動作しない。
First, in the case of normal reception, antenna 2 shown in Figure 1
The positions of the two mirror surfaces are as follows: When the focal point of the main reflecting mirror 1 is 02 and the equivalent focal point determined by the radiation characteristics of the primary radiator is O7, the two focal points OI and 02 of the sub-reflecting mirror 1-1 are the concomitant focal point. It is a hyperboloid of rotation. In this case, the main reflector 1
The radio waves radiated from are radiated to the outside in a parallel state. On the other hand, the radio wave (2) received in the child-rearing state is reflected by the main reflection @1 and the sub-reflection mirror '4, and is focused at point 02. Then, the collected radio waves are applied to the receiver RX through the feeder 7, where they are amplified by 9 frequency conversion, demodulated, and the extracted demodulated waves are taken out from the terminal 1, but the signal frequency band to be transmitted is For example, noise components and pilot signals contained in the upper frequency band are added to the reception level detector P/N. Here, the level of the miscellaneous component and pilot signal is detected and determined.The reception level is determined by comparing it with the level of the noise component and pilot signal corresponding to the reception level (for example, a level below the standard reception level). If the received level is also higher than the received level, the output of the received level detector P/N is 0 and the motor 5 does not operate.

従って電波■より外側の電波は受信せず、この空中線の
ビーム巾は最も狭い状態で電波を捕捉している。
Therefore, it does not receive radio waves outside the radio wave (■), and the antenna captures the radio waves with its narrowest beam width.

次に、ダクト性フェージングが発生して受信部入力レベ
ルが標準受信レベルよりも低下した場合は受信入力レベ
ルに対応して受信部RXから取シ出される雑音成分はレ
ベルが高くなシ、パイロット信号の信号対雑音比は小さ
く々る。このような雑音成分及びパイロット信号が受信
レベル検出器P/Nに加えられるとこの検出器で雑音成
分及びパイロット信号の信号対雑音比から現在の受信レ
ベルが定められた受信レベル以下になっていることが判
る。そして現在の受信レベルが時間1以上継続して定め
られた受信レベル以下になっていることを受信レベル検
出器P/Nが検出すると、この定められた受信レベルと
の差に対応する出力がこの検出器P/Nからモータ5に
送られる。
Next, when duct fading occurs and the input level of the receiving section falls below the standard receiving level, the noise component extracted from the receiving section RX corresponding to the receiving input level will not have a high level, but the pilot signal The signal-to-noise ratio of is small. When such noise components and pilot signals are added to the reception level detector P/N, this detector determines from the signal-to-noise ratio of the noise components and pilot signals that the current reception level is below the predetermined reception level. I understand that. When the reception level detector P/N detects that the current reception level has been below the predetermined reception level for a period of time 1 or more, the output corresponding to the difference from the predetermined reception level is It is sent to the motor 5 from the detector P/N.

モータ5はこの出力によって回転しクランク機構部6で
この回転運動が直線運動に変換され副反射鏡支柱43は
副反射鏡4を主反射鏡面1の方向に押し出すように動く
。このとき副反射鏡平面に設けられた3本の副反射鏡柱
41は支柱33の中空部をガイドにしているので、副反
射鏡面4の動きが滑らかに且つ平行移動の状態で主反射
鏡面に近ずくことになる。
The motor 5 is rotated by this output, and the crank mechanism 6 converts this rotational motion into a linear motion, and the sub-reflector column 43 moves to push the sub-reflector 4 toward the main reflector surface 1. At this time, the three sub-reflecting mirror columns 41 provided on the sub-reflecting mirror plane use the hollow portions of the pillars 33 as guides, so that the sub-reflecting mirror surface 4 moves smoothly and in parallel to the main reflecting mirror surface. It's coming soon.

これによって空中線のビーム巾は広がシミ波■も捕捉可
能となる。そして受信レベルが定められた受信レベル以
上になればその点でモータ5は停止副反射鏡4の移動は
停止する。
This expands the beam width of the antenna and makes it possible to capture stain waves. When the reception level reaches a predetermined reception level or higher, the motor 5 stops at that point and the movement of the sub-reflector 4 is stopped.

このような空中線の状態で受信していて再び受信レベル
が屍められた値以下になった場合、副反射鏡4の位置は
電波■を受信する状態に戻されこの位置から前記のよう
に副反射鏡4を移動させるろ(f) 発明の詳細 な説明したように、本発明によれば副反射鏡を移動させ
ることえより空中線のビーム巾が広がp1ダクト性フェ
ージングにより電波の伝播経路が空中線から逃げて行く
電波を捕捉することが可能にした。
If the reception level falls below the dead value again while receiving in such an antenna state, the position of the sub-reflector 4 is returned to the state in which it receives radio waves, and from this position the sub-reflector 4 is redirected from this position as described above. Move the reflecting mirror 4 (f) As described in detail, according to the present invention, by moving the sub-reflecting mirror, the beam width of the antenna is expanded and the radio wave propagation path is changed due to p1 duct-related fading. This made it possible to capture radio waves escaping from the antenna.

そこで従来のよう罠受信機、空中線等が別に一系列必要
であったダクト性フェージング対策に比較して一系列余
分な機器は不要になるので装置構成が容易になし又価格
も大巾に低下する等簡単な変更で大きな効果かえられる
Therefore, compared to conventional duct-based fading countermeasures that require a separate series of trap receivers, antennas, etc., one series of extra equipment is not required, making the equipment configuration easier and the price significantly reduced. A simple change can have a big effect.

【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を説明するだめの図である。 図中、1は主反射鏡面、2は1次放射器、3け副尺#、
I鏡取付支柱、4は副反射鏡、5はモータ、6はクラン
ク機構部、71−1:フィーダ、RXは受信部、P/N
は受信レベル検出器、OUTは端子をそれぞノ1.示す
。 第1図 U7
FIG. 1 is a diagram for explaining one embodiment of the present invention. In the figure, 1 is the main reflecting mirror surface, 2 is the primary radiator, 3-digit vernier #,
I mirror mounting column, 4 is the sub-reflector, 5 is the motor, 6 is the crank mechanism section, 71-1: feeder, RX is the receiving section, P/N
is the reception level detector, and OUT is the terminal in No. 1. show. Figure 1 U7

Claims (1)

【特許請求の範囲】[Claims] 主反射鏡、副反射鏡、1次放射器などから構成された空
中線に於て、該空中線で受信した受信レベルが一定時間
継続して定められた値以下になっていることを検知する
手段と、該検知手段からの出力で複数の副反射鏡支柱に
よシ固定された円板上に設置#された副反射鏡駆動iを
制御する手段と、制御された該副反射鏡駆動部により該
副反射鏡を平行移動する手段とからなることを特徴とす
るビーム中可変空中線。
means for detecting, in an antenna comprising a main reflector, a sub-reflector, a primary radiator, etc., that the reception level received by the antenna remains below a predetermined value for a certain period of time; , a means for controlling a sub-reflector drive i installed on a disk fixed to a plurality of sub-reflector supports using the output from the detection means; and means for moving the sub-reflector in parallel.
JP10716583A 1983-06-15 1983-06-15 Beam width variable antenna Pending JPS60103A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10716583A JPS60103A (en) 1983-06-15 1983-06-15 Beam width variable antenna

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10716583A JPS60103A (en) 1983-06-15 1983-06-15 Beam width variable antenna

Publications (1)

Publication Number Publication Date
JPS60103A true JPS60103A (en) 1985-01-05

Family

ID=14452129

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10716583A Pending JPS60103A (en) 1983-06-15 1983-06-15 Beam width variable antenna

Country Status (1)

Country Link
JP (1) JPS60103A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62128202A (en) * 1985-11-28 1987-06-10 Mitsubishi Electric Corp Sub-reflector drive device
SG110022A1 (en) * 2002-02-15 2005-04-28 Ntt Docomo Inc A radio receiver and receiving method for controlling the beam-width of an antenna

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62128202A (en) * 1985-11-28 1987-06-10 Mitsubishi Electric Corp Sub-reflector drive device
SG110022A1 (en) * 2002-02-15 2005-04-28 Ntt Docomo Inc A radio receiver and receiving method for controlling the beam-width of an antenna
US7046965B2 (en) 2002-02-15 2006-05-16 Ntt Docomo, Inc. Radio receiver and receiving method for controlling the beam-width of an antenna

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