JPS61147622A - Mobile communication system - Google Patents

Mobile communication system

Info

Publication number
JPS61147622A
JPS61147622A JP59270190A JP27019084A JPS61147622A JP S61147622 A JPS61147622 A JP S61147622A JP 59270190 A JP59270190 A JP 59270190A JP 27019084 A JP27019084 A JP 27019084A JP S61147622 A JPS61147622 A JP S61147622A
Authority
JP
Japan
Prior art keywords
base station
communication
horizontal direction
aircraft
main lobe
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
JP59270190A
Other languages
Japanese (ja)
Inventor
Yoshio Ebine
佳雄 恵比根
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.)
Nippon Telegraph and Telephone Corp
Original Assignee
Nippon Telegraph and Telephone Corp
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 Nippon Telegraph and Telephone Corp filed Critical Nippon Telegraph and Telephone Corp
Priority to JP59270190A priority Critical patent/JPS61147622A/en
Publication of JPS61147622A publication Critical patent/JPS61147622A/en
Pending legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/24Radio transmission systems, i.e. using radiation field for communication between two or more posts
    • H04B7/26Radio transmission systems, i.e. using radiation field for communication between two or more posts at least one of which is mobile

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Mobile Radio Communication Systems (AREA)

Abstract

PURPOSE:To improve the ratio of a desired wave to a distrubing ratio to a land mobile station by providing an array antenna where a directivity within a vertical plane has two upper/lower main lobes in the horizontal direction and has no sensitivity in the horizontal direction to a base station to reduce fading to an aircraft. CONSTITUTION:The directivity characteristic in the vertical plane of a base station use array antenna 2 has two main lobes 31, 31' at the lower and upper side in the horizontal direction and has no sensitivity in the horizontal direction, the upper main lobe 31 is used for an aircraft telephone subscriber 4 for communication and the lower main lobe 31' is used for an automobile telephone subscriber 5. The depression angle of the main lobe 31' is set to have the maximum gain at slightly inner side from a radio zone peripheral part of the said radio base station 1. Thus, the communication between the base station 1 and the subscriber 4 reduces fading due to reflection on sea surface and the communication with the subscriber 5 is improved for the ratio of desired wave to disturbed wave.

Description

【発明の詳細な説明】 発明の属する技術分野 本発明は、1つの基地局が航空機および陸上移動局と通
信を行なうことができる移動通信方式に関する。
DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to a mobile communication system in which one base station can communicate with aircraft and land mobile stations.

発明の概要 本発明は、航空機および陸上移動局と1つの基地局間で
通信を行なう移動通信方式において、基地局アンテナの
垂直面内指向特性を水平方向に対して上側と下側に2つ
の主ローブを持つように構成して、航空機との通信は上
側の主ローブを使用し、陸上移動局との通信は下側の主
ローブを使用することにより、航空機との通信は海面反
射等の影響によるフェージングを軽減し、陸上局との通
信は希望波と妨害波の比を改善して周波数の有効利用を
図ることができるようにしたものである。
Summary of the Invention The present invention provides two main types of vertical directivity characteristics of a base station antenna, upper and lower with respect to the horizontal direction, in a mobile communication system in which communication is performed between an aircraft, a land mobile station, and one base station. The upper main lobe is used for communication with aircraft, and the lower main lobe is used for communication with land mobile stations, so communication with aircraft is free from the effects of sea surface reflections, etc. By reducing the fading due to radio waves and improving the ratio of desired waves to interfering waves in communication with land stations, it is possible to effectively utilize frequencies.

従来技術 従来、1つの無線基地局と、航空機および自動車電話等
の陸上移動局間で通信を行なうような移動通信方式にお
いては、第5図に示すように、無線基地局1の基地゛局
用アンテナ2の指向特性3が水平方向に対して最大利得
となるようにして、航空機電話加入者4および自動車電
話加入者5と通信を行なっている。指向特性が3′とな
るようにすると、航空機電話加入者4との通信電波が微
弱となるからである。
BACKGROUND ART Conventionally, in a mobile communication system in which communication is carried out between one radio base station and land mobile stations such as aircraft and car telephones, as shown in FIG. Communication is carried out with an aircraft telephone subscriber 4 and a car telephone subscriber 5 so that the directivity characteristic 3 of the antenna 2 has a maximum gain in the horizontal direction. This is because if the directivity characteristic is set to 3', the communication radio waves with the aircraft telephone subscriber 4 will be weak.

従来技術の問題点 、上述の従来方式は、指向特性3の指向性が水平方向に
対して最大であるため、遠距離まで電波が伝搬される。
Problems with the Prior Art: In the conventional method described above, the directivity of the directional characteristic 3 is maximum in the horizontal direction, so radio waves are propagated over long distances.

このことは、大ゾーン構成の移動通信方式に対しては有
効であるが、他の基地局が同一・周波数のチャネルを繰
返し使用して自局ゾーン内の自動車電話加入者と通信す
るような小ゾーン構成の自動車電話方式等の移動通信方
式では、希望波と妨害波の比を劣化させることになると
いう欠点がある0例えば、amゾーン半径を3Kmとし
、基地局用アンテナ2の高さを100 mとし、その垂
直面内生偏角3°とした場合、無線基地局lからゾーン
周辺を見た俯角は1.9°となるから。
This is effective for mobile communication systems with large zone configurations, but for small base stations where other base stations repeatedly use the same frequency channel to communicate with mobile phone subscribers within their own zone. Mobile communication systems such as car telephone systems with zone configurations have the disadvantage of deteriorating the ratio of desired waves to interference waves.For example, if the am zone radius is 3 km and the height of the base station antenna 2 is 100 km If the angle of declination in the vertical plane is 3°, then the angle of depression when looking around the zone from the wireless base station l is 1.9°.

指向特性3の最大利得方向が自局ゾーン内に無く、むし
ろ同一周波数を繰返し使用する他の地域に最大利得が生
じるからである。
This is because the maximum gain direction of the directivity characteristic 3 is not within the own station zone, but rather the maximum gain occurs in other areas where the same frequency is repeatedly used.

また、航空機との通信は、海面反射等によるフェージン
グを伴なうという欠点がある。
Furthermore, communication with aircraft has the disadvantage that it is accompanied by fading due to reflections on the sea surface and the like.

なお、小ゾーン構成の移動通信方式において希望波と妨
害波の比を改善するためには、第5図の指向特性3′の
ようにビームチルティングさせて、無線ゾーン周辺部に
最大利得を生じるような指向特性にすることが望ましい
が、その場合は航空機電話加入者4との通信電波が微弱
になって通信ができなくなる。
In addition, in order to improve the ratio of desired waves to interference waves in a mobile communication system with a small zone configuration, beam tilting is performed as shown in directional characteristic 3' in Figure 5 to produce maximum gain at the periphery of the wireless zone. Although it is desirable to have such a directional characteristic, in that case, the communication radio waves with the aircraft telephone subscriber 4 become weak and communication becomes impossible.

発明の目的 本発明の目的は、上述の従来の欠点を解決し、航空機と
の通信は海面反射の影響によるフェージングを軽減し、
陸上移動局との通信は希望波と妨害波の比を改善して周
波数の有効利用を図ることができる移動通信方式を提供
することにある。
OBJECTS OF THE INVENTION The purpose of the present invention is to solve the above-mentioned conventional drawbacks, and to reduce fading caused by the influence of sea surface reflections in communications with aircraft;
The purpose of communication with land mobile stations is to provide a mobile communication system that can improve the ratio of desired waves to interference waves and effectively utilize frequencies.

発明の構成 本発明の移動通信方式は、航空機および陸上移動局と基
地局間にそれぞれ割当てられたチャネルによって通信を
行なう移動通信方式において、前記基地局は、垂直面内
指向特性が水平方向に対して上側と下側に2つの主ロー
ブを持ち水平方向には感度を有しないアレイアンテナを
備えて、航空機との通信は上側の主ローブを使用し、陸
上移動局との通信は下側の主ローブを使用して行なうこ
とを特徴とする。
Composition of the Invention The mobile communication system of the present invention is a mobile communication system in which communication is performed between an aircraft, a land mobile station, and a base station through channels respectively allocated to the base station. It is equipped with an array antenna that has two main lobes on the upper and lower sides and has no sensitivity in the horizontal direction. Communication with aircraft uses the upper main lobe, and communication with land mobile stations uses the lower main lobe. It is characterized by using a robe.

発明の実施例 次に1本発明について1図面を参照して詳細に説明する
Embodiments of the Invention Next, one embodiment of the present invention will be described in detail with reference to one drawing.

第1図は、本発明の一実施例を示す概念図である。すな
わち、基地局用アンテナ2の垂直面内指向特性が水平方
向の上側と下側に2つの主ローブ31.31’を持つよ
うにして、上側の主ローブ31を使用して航空機電話加
入者4と通信し、下側の主ローブ31′を使用して自動
車電話加入者5と通信するようにする。主ローブ31’
の俯角は、当該無線基地局lの無線ゾーン周辺部よりや
や内側に対して最大利得となるように設定されている。
FIG. 1 is a conceptual diagram showing one embodiment of the present invention. That is, the vertical plane directivity characteristic of the base station antenna 2 has two main lobes 31 and 31' on the upper and lower sides in the horizontal direction, and the upper main lobe 31 is used to connect the aircraft telephone subscriber 4. and the lower main lobe 31' is used to communicate with the mobile phone subscriber 5. Main lobe 31'
The angle of depression is set so that the maximum gain is achieved slightly inside the periphery of the radio zone of the radio base station I.

第2図は1本実施例の基地局用アンテナ2の配列を示す
図であり、8個のアンテナ素子A1〜A8を垂直に素子
間隔りが1波長λとなるように配列した素子群のすべて
のアンテナ素子A!〜A8を同相給電とし、同様な8個
のアンテナ素子AI  ’〜A8 ’には逆相給電する
ようにし、上記2つの素子群の中心間隔Sが8λとなる
ように上下2段に配置している。各アンテナ素子は、例
えばダイポールアンテナで構成されている。
FIG. 2 is a diagram showing the arrangement of the base station antenna 2 of this embodiment, in which all eight antenna elements A1 to A8 are arranged vertically so that the element spacing is one wavelength λ. Antenna element A! ~A8 is fed in-phase, and eight similar antenna elements AI'~A8' are fed in reverse phase, and arranged in upper and lower two stages so that the center spacing S between the two element groups is 8λ. There is. Each antenna element is composed of, for example, a dipole antenna.

第3図は、上記基地局用アンテナ2の垂直面内指向特性
を示す図であり、横軸・には水平方向に対する仰角また
は俯角を、縦軸には指向特性を示す、すなわち、水平方
向に対して上2゜5°の方向に最大利得の主ローブを有
する。
FIG. 3 is a diagram showing the directivity characteristics in the vertical plane of the base station antenna 2, where the horizontal axis shows the elevation angle or depression angle with respect to the horizontal direction, and the vertical axis shows the directivity characteristics, that is, the horizontal direction. It has a main lobe of maximum gain in the direction of 2°5° above.

木実流側においては、無線基地局1と航空機電話加入者
4間の通信は上側の主ローブ31t−使用し、自動車電
話加入者5との通信は下側の主ローブ31’を使用して
行なう、従って、例えば基地局用アンテナ2の高さを1
00mとし、航空機の高度を10Kmとし、無線ゾーン
の半径を3Kmとした場合、航空機に対する最大利得方
向は+2.5 °であるから、約230に■の位置にあ
る航空機比対して最大利得を与え、目標ゾーンをカバー
することができる。また、航空機からの電波が地上の建
造物等によって水平方向に朱じた散乱波は、アンテナ指
向特性によって軽減されるため、フェージングが緩和さ
れることになる。
On the wood flow side, communication between the radio base station 1 and the aircraft telephone subscriber 4 uses the upper main lobe 31t, and communication with the car telephone subscriber 5 uses the lower main lobe 31'. Therefore, for example, the height of the base station antenna 2 is
00m, the altitude of the aircraft is 10Km, and the radius of the radio zone is 3Km. Since the maximum gain direction for the aircraft is +2.5 degrees, the maximum gain for the aircraft at the position of approximately 230 is given. , can cover the target zone. In addition, scattered waves caused by radio waves from an aircraft being distorted in the horizontal direction by buildings on the ground, etc. are reduced by the antenna directivity characteristics, so fading is alleviated.

一方、主ローブ3Fの水平方向に対する角度は−2,5
°であるから、最大利得の方向は無線ゾーンの周辺部よ
りやや内側を指向することになる。
On the other hand, the angle of the main lobe 3F with respect to the horizontal direction is -2,5
°, the direction of maximum gain is directed slightly inside the periphery of the wireless zone.

第4図は、II!1線基地局1からの距離と地上での受
信レベルの関係を示す図であり、実線で示した曲線aは
本実施例の特性を示し、破線で示した曲線すは従来の特
性を示す、すなわち1本実施例は、3に層以内のゾーン
内では従来よりも受信レベルが向Hし、3に層を越えた
ゾーン外では従来よりも受信レベルが低下する。しかも
、レベル低下の度合は、距離が大きくなる程大きくなっ
ている0例えば、希望波と妨害波の比が20dB以上必
要であるとすると、従来は20に層以上離れた地域でな
いと同一の周波数を鰻返して使用することができないが
、本実施例では約9に腸まで短編することができる。
Figure 4 shows II! It is a diagram showing the relationship between the distance from the 1-line base station 1 and the reception level on the ground, where the curve a shown by a solid line shows the characteristics of this embodiment, and the curve shown by a broken line shows the conventional characteristics. That is, in this embodiment, the reception level is higher than the conventional one within the zone within the third layer, and the reception level is lower than the conventional one outside the zone beyond the third layer. Moreover, the degree of level reduction increases as the distance increases.For example, if the ratio of the desired signal to the interfering signal is required to be 20 dB or more, conventionally, unless the area is more than 20 layers away, the same frequency However, in this example, it is possible to shorten the length of the eel to approximately 9 mm.

発明の効果 以上のように、本発明においては、航空機に対してはフ
ェージングを軽減し、陸上移動局に対しては希望波と妨
害波の比を改善できるという効果があり、またこれに伴
って周波数の利用効率を向上することができるいう効果
がある。
Effects of the Invention As described above, the present invention has the effect of reducing fading for aircraft and improving the ratio of desired waves to interference waves for land mobile stations. This has the effect of improving frequency usage efficiency.

【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示す概念図、第2図は上記
実施例の基地局用アンテナの配列の一例を示す図、第3
図は上記基地局用アンテナの垂直面内指向特性を示す図
、第4図は上記実施例および従来例における基地局から
の距離と地上受信レベルの関係を示す図、第5図は従来
の移動通信方式の一例を示す概念図である。 図において、1:無線基地局、2二基地局用アンテナ、
3.3’:従来例の指向特性、4:航空機電話加入者、
5:自動車電話加入者、31゜31′:主ローブ。
FIG. 1 is a conceptual diagram showing one embodiment of the present invention, FIG. 2 is a diagram showing an example of the array of base station antennas of the above embodiment, and FIG.
The figure shows the directivity characteristics in the vertical plane of the base station antenna, FIG. 4 shows the relationship between the distance from the base station and the ground reception level in the above embodiment and the conventional example, and FIG. FIG. 2 is a conceptual diagram showing an example of a communication method. In the figure, 1: wireless base station, 22: base station antenna,
3.3': Directional characteristics of conventional example, 4: Aircraft telephone subscriber,
5: Car phone subscriber, 31°31': Main lobe.

Claims (1)

【特許請求の範囲】[Claims] 航空機および陸上移動局と基地局間にそれぞれ割当てら
れたチャネルによつて通信を行なう移動通信方式におい
て、前記基地局は、垂直面内指向特性が水平方向に対し
て上側と下側に2つの主ローブを持ち水平方向には感度
を有しないアレイアンテナを備えて、航空機との通信は
上側の主ローブを使用し、陸上移動局との通信は下側の
主ローブを使用して行なうことを特徴とする移動通信方
式。
In a mobile communication system in which communication is performed between an aircraft or a land mobile station and a base station through channels respectively allocated, the base station has two main vertical directivity characteristics, one above and the other below the horizontal direction. Equipped with an array antenna that has lobes and is not sensitive in the horizontal direction, communication with aircraft is performed using the upper main lobe, and communication with land mobile stations is performed using the lower main lobe. mobile communication system.
JP59270190A 1984-12-21 1984-12-21 Mobile communication system Pending JPS61147622A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59270190A JPS61147622A (en) 1984-12-21 1984-12-21 Mobile communication system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59270190A JPS61147622A (en) 1984-12-21 1984-12-21 Mobile communication system

Publications (1)

Publication Number Publication Date
JPS61147622A true JPS61147622A (en) 1986-07-05

Family

ID=17482773

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59270190A Pending JPS61147622A (en) 1984-12-21 1984-12-21 Mobile communication system

Country Status (1)

Country Link
JP (1) JPS61147622A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100784643B1 (en) 2006-07-25 2007-12-12 에스케이 텔레콤주식회사 Method and apparatus for providing mobile communication service on the ocean and system including the apparatus
JP2009217460A (en) * 2008-03-10 2009-09-24 Nec Corp Measurement system, buoy, receiver and measurement method
JP2017523742A (en) * 2014-05-28 2017-08-17 ルフトハンザ・ジステムズ・ゲゼルシャフト・ミットベシュレンクテル・ハフツング・ウント・コンパニ・コマンディートゲゼルシャフトLufthansa Systems Gmbh & Co. Kg Apparatus and method for aircraft air-to-ground communication

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100784643B1 (en) 2006-07-25 2007-12-12 에스케이 텔레콤주식회사 Method and apparatus for providing mobile communication service on the ocean and system including the apparatus
JP2009217460A (en) * 2008-03-10 2009-09-24 Nec Corp Measurement system, buoy, receiver and measurement method
JP2017523742A (en) * 2014-05-28 2017-08-17 ルフトハンザ・ジステムズ・ゲゼルシャフト・ミットベシュレンクテル・ハフツング・ウント・コンパニ・コマンディートゲゼルシャフトLufthansa Systems Gmbh & Co. Kg Apparatus and method for aircraft air-to-ground communication

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