JP2615769B2 - Direction measurement device - Google Patents
Direction measurement deviceInfo
- Publication number
- JP2615769B2 JP2615769B2 JP5110488A JP5110488A JP2615769B2 JP 2615769 B2 JP2615769 B2 JP 2615769B2 JP 5110488 A JP5110488 A JP 5110488A JP 5110488 A JP5110488 A JP 5110488A JP 2615769 B2 JP2615769 B2 JP 2615769B2
- Authority
- JP
- Japan
- Prior art keywords
- antenna
- reception
- trigger
- directional
- 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
Links
Landscapes
- Radar Systems Or Details Thereof (AREA)
Description
【発明の詳細な説明】 〔産業上の利用分野〕 本発明は方位測定装置に関し、特に到来したパルス電
波を測定対象としてその方位を測定する場合に必要とな
るパルス電波信号に対するA−D変換処理の改善を図っ
た方位測定装置に関する。Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an azimuth measuring apparatus, and more particularly to an A / D conversion process for a pulse radio signal required when measuring an azimuth of an incoming pulse radio wave as a measurement target. The present invention relates to a direction measuring device that improves the above.
〔従来の技術〕 従来、この種の方位測定装置は、例えば第2図に示す
様に、指向性空中線1a,1b,1c,1dおよび1e、受信回路3a,
3b,3c,3dおよび3e、A−D変換回路5a,5b,5c,5dおよび5
eをそれぞれ組として有し、方位処理回路7で各指向性
空中線で受信した信号の振幅を比較し、まず振幅が最大
となる指向性空中線の方向から大体の方位を求め、さら
にこの最大振幅の指向性空中線と隣接する指向性空中線
について両者の受信信号の振幅比を求め、さらにこの振
幅比から電波の到来方向が指向性空中線間のどこに位置
するかを内挿によって求め正確な方位を得ている。[Prior Art] Conventionally, this type of azimuth measuring apparatus has, for example, as shown in FIG. 2, directional antennas 1a, 1b, 1c, 1d and 1e, receiving circuits 3a,
3b, 3c, 3d and 3e, A / D conversion circuits 5a, 5b, 5c, 5d and 5
e as a set, and the azimuth processing circuit 7 compares the amplitudes of the signals received by the respective directional antennas. First, an approximate azimuth is obtained from the direction of the directional antenna having the largest amplitude. For the directional antenna and the adjacent directional antenna, determine the amplitude ratio of the received signals of both, and from this amplitude ratio find the position of the incoming radio wave between the directional antennas by interpolation to obtain the correct azimuth. I have.
この場合、到来する電波がパルス電波の場合には、こ
のパルス電波による受信パルス信号の振幅を量子化する
必要があるが、この目的のため無指向性空中線2とこれ
に接続する受信回路4を用意し、この出力を利用して振
幅量子化のためのトリガ信号をトリガ発生回路8で作り
出し、A−D変換回路5a−5eに供給している。In this case, if the arriving radio wave is a pulse radio wave, it is necessary to quantize the amplitude of the received pulse signal by the pulse radio wave. For this purpose, the omnidirectional antenna 2 and the receiving circuit 4 connected thereto are connected. A trigger signal for amplitude quantization is generated by the trigger generation circuit 8 using this output, and is supplied to the A / D conversion circuits 5a to 5e.
上述した従来の方位測定装置では、正確な方位を求め
るためには正確なトリガタイミングで量子化を行う必要
があるが、指向性空中線を配置する場合にはある程度の
空間的広がりが生じることと、さらに、指向性空中線と
無指向性空中線との間にはある程度距離があることか
ら、到来電波の方向によって指向性空中線と無指向性空
中線との間で電波が到達する時刻に差を生じて量子化に
おけるトリガタイミングに誤差が生じるため、とくに狭
いパルス幅の到来電波の場合には十分な精度を保持した
振幅量子化を行いにくいと言う欠点がある。In the above-described conventional azimuth measuring apparatus, it is necessary to perform quantization at an accurate trigger timing in order to obtain an accurate azimuth.However, when a directional antenna is arranged, a certain degree of spatial spread occurs, Furthermore, since there is a certain distance between the directional antenna and the omnidirectional antenna, there is a difference in the time at which the radio waves arrive between the directional antenna and the omnidirectional antenna, depending on the direction of the arriving radio wave. Since an error occurs in the trigger timing in the quantization, there is a drawback that it is difficult to perform the amplitude quantization with sufficient accuracy particularly in the case of an incoming radio wave having a narrow pulse width.
本発明の装置は、所定の角度間隔で平面に配列した複
数の指向性空中線と、無指向性空中線と、前記指向性空
中線及び無指向性空中線にそれぞれに接続された受信回
路と、到来したパルス電波を受信した時前記無指向性空
中線に接続された受信回路が出力する受信信号からトリ
ガ信号を作り出すトリガ発生回路と、前記指向性空中線
に接続された受信回路にそれぞれ接続され前記パルス電
波による受信信号の振幅を前記トリガ信号のタイミング
で読み取り量子化するA−D変換回路と、このA−D変
換回路のそれぞれが出力する量子化受信振幅のうち最大
の受信振幅を提供する前記指向性空中線の方向及びこれ
と隣接する指向性空中線による受信振幅の比から前記到
来したパルス電波の方位を求めて出力する方位処理回路
とからなる方位測定装置において、前記トリガ発生回路
を前記無指向性空中線に接続された受信回路出力を共通
入力とし出力で前記A−D変換回路のそれぞれをトリガ
する複数個のトリガ発生回路として構成するとともにそ
れぞれのトリガ発生回路内におけるトリガ遅延時間は対
応する前記指向性空中線の指向方向から前記パルス電波
が到来する時に前記無指向性空中線との位置の差によっ
て生じる到来時間差に対応したものに設定した構成を有
する。The apparatus of the present invention comprises a plurality of directional antennas arranged in a plane at predetermined angular intervals, an omnidirectional antenna, receiving circuits respectively connected to the directional antenna and the omnidirectional antenna, and an incoming pulse. When a radio wave is received, a trigger generation circuit that generates a trigger signal from a reception signal output by a reception circuit connected to the omnidirectional antenna, and reception by the pulse radio wave respectively connected to a reception circuit connected to the directional antenna An A / D conversion circuit for reading and quantizing the signal amplitude at the timing of the trigger signal, and the directional antenna for providing the maximum reception amplitude among the quantized reception amplitudes output from each of the A / D conversion circuits. An azimuth processing circuit for obtaining and outputting the azimuth of the arriving pulse radio wave from the direction and the ratio of the reception amplitude of the adjacent directional antenna to the azimuth; Wherein the trigger generation circuit is configured as a plurality of trigger generation circuits that use the output of a reception circuit connected to the omnidirectional antenna as a common input and trigger each of the A / D conversion circuits with an output. The trigger delay time in the generation circuit is set to correspond to an arrival time difference caused by a difference in position from the omnidirectional antenna when the pulse radio wave arrives from the directional direction of the corresponding directional antenna.
次に、図面を参照して本発明を詳細に説明する。第1
図は本発明の一実施例のブロック図である。第1図に示
す実施例の構成は、指向性空中線1a,1b,1c,1dおよび1
e、無指向性空中線2、受信回路3a,3b,3c,3dおよび3e,
4、A−D変換回路5a,5b,5c,5dおよび5e、トリガ回路発
生回路6a,6b,6c,6dおよび6e、方位処理回路7を備えて
構成され、これら構成内容のうちトリガ発生回路6a,6b,
6c,6dおよび6e以外は第2図に示す同一記号のものと同
じであるので、これら同一のものについての詳細な説明
は省略する。Next, the present invention will be described in detail with reference to the drawings. First
The figure is a block diagram of one embodiment of the present invention. The configuration of the embodiment shown in FIG. 1 includes directional antennas 1a, 1b, 1c, 1d and 1
e, omnidirectional antenna 2, receiving circuits 3a, 3b, 3c, 3d and 3e,
4, an AD conversion circuit 5a, 5b, 5c, 5d and 5e, a trigger circuit generation circuit 6a, 6b, 6c, 6d and 6e, and an azimuth processing circuit 7; , 6b,
Elements other than 6c, 6d and 6e are the same as those shown in FIG. 2 and the detailed description of these same elements will be omitted.
本実施例の方位測定装置は、従来の1個のトリが発生
回路でトリガ信号を発生しA−D変換回路5a〜5eのそれ
ぞれに供給しているのに対し、第1図の如く、指向性空
中線1a〜1eのそれぞれに対応した複数、第1図の場合は
5個のトリガ発生回路6a〜6eで構成している。In the azimuth measuring apparatus of the present embodiment, a conventional bird generates a trigger signal in a generating circuit and supplies the trigger signal to each of the AD converting circuits 5a to 5e. It comprises a plurality of trigger generating circuits 6a to 6e corresponding to the respective antennas 1a to 1e, in the case of FIG.
さらに、これら複数のトリガ発生回路の遅延時間は、
それぞれが対応する指向性空中線の指向方位にもとづ
き、パルス電波が到来したときに無指向性空中線2との
距離によって生ずる遅延時間に対応して設定される。第
1図の場合、指向性空中線1bについて言えば、その指向
方向と一致するパルス電波到来方向に対する無指向性空
中線2との受信処理差,すなわち距離Lに対応する遅延
時間がトリガ発生回路6bに付与されることとなる。この
ように、各指向性空中線に付与される遅延時間は、無指
向性空中線2ならびに各指向性空中線1a〜1eの配列条件
にもとづき、各指向性空中線のそれぞれに対応する指向
方位からパルス電波が到来したときの無指向性空中線と
の距離差に対応するものとしてあらかじめ設定される。Furthermore, the delay time of these multiple trigger generation circuits is
Based on the directional azimuths of the corresponding directional antennas, they are set according to the delay time caused by the distance from the omnidirectional antenna 2 when a pulse radio wave arrives. In the case of FIG. 1, regarding the directional antenna 1b, the reception processing difference between the directional antenna 1 and the omnidirectional antenna 2 with respect to the direction of arrival of the pulse radio wave, that is, the delay time corresponding to the distance L is transmitted to the trigger generation circuit 6b. Will be granted. In this way, the delay time given to each directional antenna is based on the omnidirectional antenna 2 and the arrangement conditions of the directional antennas 1a to 1e, and the pulse radio waves are transmitted from the directional directions corresponding to each directional antenna. It is set in advance to correspond to the distance difference from the omnidirectional antenna when it arrives.
このようにして、電波到来方向あるいはその付近の方
向を向いた指向性空中線については遅延時間の差が補正
される。In this way, the difference in delay time is corrected for a directional antenna that is oriented in the direction of arrival of a radio wave or in the vicinity thereof.
なお、電波到来方向と離れた方位に向いた指向性空中
線については遅延時間は補正されないが、方位測定に使
用するのは電波の到来方向に指向した指向性空中線及び
その周辺のみであるため、これから離れた指向性空中線
で生じるトリガタイミング誤差は問題とならない。Note that the delay time is not corrected for directional antennas pointing in a direction away from the direction of arrival of radio waves, but only directional antennas pointing in the direction of arrival of radio waves and their surroundings are used for azimuth measurement. Trigger timing errors occurring in distant directional antennas are not a problem.
以上説明したように本発明によれば、無指向性空中線
と複数の指向性空中線を利用して方位測定を行なう従来
の方位測定装置における1個のトリガ発生回路のかわり
に指向性空中線に対応した複数のトリガー回路を備えた
うえ、各指向性空中線の指向方向から到来するパルス電
波に対しては、無指向性空中線との伝搬距離差に対応す
る遅延時間を付与してこれを量子化することにより、パ
ルス電波到来方向もしくはその付近を指向する指向性空
中線については無指向性空中線との電波到来時間差によ
る量子化トリガタイミング差を十分に補正しうるという
効果がある。As described above, according to the present invention, a directional antenna is used instead of a single trigger generation circuit in a conventional azimuth measuring device that performs azimuth measurement using an omnidirectional antenna and a plurality of directional antennas. In addition to providing multiple trigger circuits, pulse radio waves arriving from the directional direction of each directional antenna should be quantized with a delay time corresponding to the propagation distance difference from the omnidirectional antenna. Thus, for a directional antenna that points in or near the direction of arrival of the pulse radio wave, the quantization trigger timing difference due to the radio wave arrival time difference from the non-directional antenna can be sufficiently corrected.
【図面の簡単な説明】 第1図は本発明の一実施例のブロック図、第2図は従来
の方位測定装置のブロック図である。 1a,1b,1c,1d,1e……指向性空中線、2……む指向性空中
線、3a,3b,3c,3d,3e,4……受信回路、5a,5b,5c,5d,5e…
…A−D変換回路、6a,6b,6c,6d,6e,7……方位処理回
路、8……トリガ発生回路。BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a block diagram of one embodiment of the present invention, and FIG. 2 is a block diagram of a conventional direction measuring device. 1a, 1b, 1c, 1d, 1e ... directional antenna, 2 ... directional antenna, 3a, 3b, 3c, 3d, 3e, 4 ... receiving circuit, 5a, 5b, 5c, 5d, 5e ...
... A / D conversion circuit, 6a, 6b, 6c, 6d, 6e, 7 ... azimuth processing circuit, 8 ... trigger generation circuit.
Claims (1)
向性空中線と、無指向性空中線と、前記指向性空中線及
び無指向性空中線にそれぞれに接続された受信回路と、
到来したパルス電波を受信した時前記無指向性空中線に
接続された受信回路が出力する受信信号からトリガ信号
を作り出すトリガ発生回路と、前記指向性空中線に接続
された受信回路にそれぞれ接続され前記パルス電波によ
る受信信号の振幅を前記トリガ信号のタイミングで読み
取り量子化するA−D変換回路と、このA−D変換回路
のそれぞれが出力する量子化受信振幅のうち最大の受信
振幅を提供する前記指向性空中線の方向及びこれと隣接
する指向性空中線による受信振幅の比から前記到来した
パルス電波の方位を求めて出力する方位処理回路とから
なる方位測定装置において、 前記トリガ発生回路を前記無指向性空中線に接続された
受信回路出力を共通入力とし出力で前記A−D変換回路
のそれぞれをトリガする複数個のトリガ発生回路として
構成するとともにそれぞれのトリガ発生回路内における
トリガ遅延時間は対応する前記指向性空中線の指向方向
から前記パルス電波が到来する時に前記無指向性空中線
との位置の差によって生じる到来時間差に対応したもの
に設定したことを特徴とする方位測定装置。1. A plurality of directional antennas arranged in a plane at predetermined angular intervals, an omnidirectional antenna, and receiving circuits respectively connected to the directional antenna and the omnidirectional antenna.
A trigger generation circuit that generates a trigger signal from a reception signal output by a reception circuit connected to the omnidirectional antenna when an incoming pulse radio wave is received, and the pulse connected to a reception circuit connected to the directional antenna, respectively. An A / D conversion circuit for reading and quantizing the amplitude of a reception signal by radio waves at the timing of the trigger signal; and a directivity providing the largest reception amplitude among the quantized reception amplitudes output from the respective A / D conversion circuits. An azimuth processing circuit for obtaining and outputting the azimuth of the arriving pulse radio wave from the direction of the directional antenna and the ratio of the reception amplitudes of the directional antennas adjacent thereto, and outputting the azimuth. Generating a plurality of triggers that use the output of a receiving circuit connected to an antenna as a common input and trigger each of the A / D conversion circuits with an output. When configured as a circuit, the trigger delay time in each trigger generation circuit corresponds to an arrival time difference caused by a difference in position from the omnidirectional antenna when the pulse radio wave arrives from the direction of the corresponding directional antenna. An azimuth measuring device characterized in that it is set to an object.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5110488A JP2615769B2 (en) | 1988-03-03 | 1988-03-03 | Direction measurement device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5110488A JP2615769B2 (en) | 1988-03-03 | 1988-03-03 | Direction measurement device |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH01223371A JPH01223371A (en) | 1989-09-06 |
JP2615769B2 true JP2615769B2 (en) | 1997-06-04 |
Family
ID=12877501
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP5110488A Expired - Lifetime JP2615769B2 (en) | 1988-03-03 | 1988-03-03 | Direction measurement device |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2615769B2 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0415584A (en) * | 1990-05-10 | 1992-01-20 | Nec Corp | Trigger circuit |
US5381444A (en) * | 1991-10-31 | 1995-01-10 | Fujitsu Limited | Radio environment measuring system |
-
1988
- 1988-03-03 JP JP5110488A patent/JP2615769B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPH01223371A (en) | 1989-09-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EXPY | Cancellation because of completion of term |