JPH01202935A - Space diversity reception system - Google Patents
Space diversity reception systemInfo
- Publication number
- JPH01202935A JPH01202935A JP63026564A JP2656488A JPH01202935A JP H01202935 A JPH01202935 A JP H01202935A JP 63026564 A JP63026564 A JP 63026564A JP 2656488 A JP2656488 A JP 2656488A JP H01202935 A JPH01202935 A JP H01202935A
- Authority
- JP
- Japan
- Prior art keywords
- interval
- propagation
- reception
- line
- diversity reception
- 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.)
- Granted
Links
- 238000004891 communication Methods 0.000 claims abstract description 7
- 238000000034 method Methods 0.000 claims description 4
- 238000005562 fading Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
Landscapes
- Radio Transmission System (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
この発明はマイクロ波通信回線に適用するダイバーシテ
ィ受信に関し、特にダイバーシティ受信に用いる2つの
空中線を備えたスペースダイバーシティ受信方式に関す
る。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to diversity reception applied to microwave communication lines, and more particularly to a space diversity reception system equipped with two antennas used for diversity reception.
従来、この種のスペースダイバーシティ受(Rt方式は
例えば島と島を結ぶ距離が11001a前後になるマイ
クロ波通信回線に用いられておシ、通常の等価地球半径
係数K = 4/3位のときには第3図(イ)に示すよ
うに見通し内伝搬となシ、等価地球半径係数に=273
位のときには第3図(ロ)に示すように見通し外伝搬と
なる。そのため、見通し内マイクロ波通信回線では反射
波による回線瞬断をさける九め、ダイバーシティ受信用
の2つの空中線は垂直方向に所定の間隔を設けて配置さ
れていた。−方、見通し外マイクロ波通信回線では回線
のフェージング対策としてできる限シ相関のない受信信
号を得るため、ダイバーシティ受信用の2つの空中線は
水平方向に所定の間隔を設けて配置されていた。Conventionally, this type of space diversity reception (Rt method) has been used, for example, in microwave communication lines where the distance between islands is around 11001a, and when the normal equivalent earth radius coefficient K = 4/3, As shown in Figure 3 (a), if line-of-sight propagation occurs, the equivalent earth radius coefficient = 273
When the distance is 1, the propagation occurs outside the line of sight as shown in Figure 3 (b). Therefore, in line-of-sight microwave communication lines, two antennas for diversity reception are placed at a predetermined distance in the vertical direction in order to avoid instantaneous line interruptions due to reflected waves. On the other hand, in non-line-of-sight microwave communication lines, two antennas for diversity reception are placed at a predetermined distance in the horizontal direction in order to obtain received signals with as little correlation as possible as a countermeasure against line fading.
上述した従来のスペースダイバーシティ受信方式は2つ
の空中線が垂直方向あるいは水平方向に所定の間隔を設
けて配置されているので、見通し内の伝搬または見通し
外の伝播の一方くしかダイバーシティ受信の効果が期待
できないという欠点がある。In the conventional space diversity reception method described above, two antennas are placed with a predetermined interval in the vertical or horizontal direction, so it is expected that diversity reception will only be effective in either line-of-sight propagation or non-line-of-sight propagation. The drawback is that it cannot be done.
この発明に係るスペースダイバーシティ受信方式はダイ
バーシティ受信に適用する第1の空中線と第2の空中線
を垂直方向に間隔Vでかつ水平方向に間隔Hで配置する
ものである。In the space diversity reception system according to the present invention, a first antenna and a second antenna used for diversity reception are arranged at an interval V in the vertical direction and an interval H in the horizontal direction.
この発明は電波伝搬状況が見通し内伝数となつ1)見通
し外伝搬となったシしても受信レベルの低下を最少限に
おさえることができる。According to the present invention, even if the radio wave propagation situation becomes line-of-sight propagation (1) non-line-of-sight propagation, it is possible to minimize the decrease in reception level.
第1図はこの発明に係るスペースダイバーシティ受信方
式の一実施例を示すブロック図である。FIG. 1 is a block diagram showing an embodiment of a space diversity reception system according to the present invention.
同図において、1および2はその詳細な正面図を第2図
に示すように垂直方向の間隔がVでかつ水平方向の間隔
がHで配置された第1空中線および第2空中線、3aお
よび3bは受信装置、4は合成装置である。In the same figure, 1 and 2 are a first antenna and a second antenna 3a and 3b arranged with a vertical interval of V and a horizontal interval of H, as shown in the detailed front view of FIG. 4 is a receiving device, and 4 is a combining device.
次に上記構成によるスペースダイバーシティ受信方式の
動作について説明する0まず、児通し内伝搬の場合には
海上などによる反射波と直接波との位相差によシ生じる
受信入力レベルの低下(瞬断を含むフェージング)をハ
イドパターンのハーフピッチの奇数倍の上下位置(間隔
V)に置かれた2つの空中線1および空中線2から得ら
れる2つの受信信号を選択することによυ受信入力レベ
ルの低下を最少限におさえることができる。一方、見通
し外伝搬の場合には常に短周期の深いフェージング(受
信入力レベルの変動)が生じているが、電波伝搬通路が
異なると、そのフェージングの相関が小さくなる(すな
わちフェージングパターンが異なる)ことを利用し、水
平方向の位置(間隔H)に置かれた2つの空中線1およ
び空中線2から得られる異なる伝搬通路の2つの受信信
号を選択することによシ受信入力レベルの低下を最少限
におさえることができる。Next, we will explain the operation of the space diversity reception system with the above configuration. First, in the case of internal propagation, the reception input level decreases due to the phase difference between the reflected wave from the ocean and the direct wave (instantaneous interruption). (including fading) by selecting two received signals obtained from two antennas 1 and 2 placed at upper and lower positions (interval V) that are odd multiples of the half pitch of the hide pattern. can be kept to a minimum. On the other hand, in the case of non-line-of-sight propagation, short-period deep fading (fluctuations in received input level) always occurs, but if the radio wave propagation path differs, the correlation of the fading becomes smaller (that is, the fading pattern differs). The reduction in the reception input level is minimized by selecting two reception signals with different propagation paths obtained from the two antennas 1 and 2 placed at horizontal positions (distance H). It can be suppressed.
以上詳細に説明したように、この発明に係るスペースダ
イバーシティ受信方式によれば、見通し内伝搬と見通し
外伝搬との2つの伝搬状況をもったマイクロ波通信回線
においてそれぞれに対応したダイバーシティ受信が得ら
れる効果がある。As explained in detail above, according to the space diversity reception method according to the present invention, diversity reception corresponding to each of the two propagation conditions, line-of-sight propagation and non-line-of-sight propagation, can be obtained in a microwave communication line. effective.
第1図はこの発明に係るスペースダイバーシティ受信方
式の一実施例を示す概略側面図、第2図は第1図の2つ
の空中線の配置を示す図、第3図(耐および第3図(b
)は各等価地球半径係数Kに対する電波伝搬状況の違い
を示す図である。
1および2・・・・空中線、3mおよび3bφ・・自受
信装置、4・・・・合成装置。
特許出願人 日本電気株式会社FIG. 1 is a schematic side view showing an embodiment of the space diversity receiving system according to the present invention, FIG. 2 is a diagram showing the arrangement of the two antennas shown in FIG.
) is a diagram showing the difference in radio wave propagation conditions for each equivalent earth radius coefficient K. 1 and 2: antenna, 3m and 3bφ: self-receiving device, 4: combining device. Patent applicant: NEC Corporation
Claims (1)
内伝搬となつたり、見通し外伝搬となつたりするような
マイクロ波通信回線において、ダイバーシティ受信に適
用する第1の空中線と第2の空中線を垂直方向に間隔V
で、かつ水平方向に間隔Hで配置することを特徴とする
スペースダイバーシティ受信方式。In microwave communication lines where the radio wave propagation status changes to line-of-sight propagation or non-line-of-sight propagation due to variations in the equivalent earth radius coefficient K, the first and second antennas used for diversity reception are vertically connected. spacing V in the direction
A space diversity reception method characterized in that the antennas are arranged at intervals of H in the horizontal direction.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63026564A JP2663478B2 (en) | 1988-02-09 | 1988-02-09 | Space diversity reception method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63026564A JP2663478B2 (en) | 1988-02-09 | 1988-02-09 | Space diversity reception method |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH01202935A true JPH01202935A (en) | 1989-08-15 |
JP2663478B2 JP2663478B2 (en) | 1997-10-15 |
Family
ID=12197034
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP63026564A Expired - Lifetime JP2663478B2 (en) | 1988-02-09 | 1988-02-09 | Space diversity reception method |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2663478B2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1115800C (en) * | 1997-09-29 | 2003-07-23 | 夸尔柯姆股份有限公司 | Using multiple antennas to mitigate specular reflection |
GB2501809A (en) * | 2012-04-26 | 2013-11-06 | Korea Electronics Telecomm | Maritime wireless communication apparatus using vertically spaced antennas to provide frequency and space diversity gain |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61121043U (en) * | 1985-01-18 | 1986-07-30 |
-
1988
- 1988-02-09 JP JP63026564A patent/JP2663478B2/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61121043U (en) * | 1985-01-18 | 1986-07-30 |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1115800C (en) * | 1997-09-29 | 2003-07-23 | 夸尔柯姆股份有限公司 | Using multiple antennas to mitigate specular reflection |
GB2501809A (en) * | 2012-04-26 | 2013-11-06 | Korea Electronics Telecomm | Maritime wireless communication apparatus using vertically spaced antennas to provide frequency and space diversity gain |
GB2501809B (en) * | 2012-04-26 | 2014-10-15 | Korea Electronics Telecomm | Maritime wireless communication apparatus and method |
Also Published As
Publication number | Publication date |
---|---|
JP2663478B2 (en) | 1997-10-15 |
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