JPS61202174A - Receiving sensitivity control circuit for radar - Google Patents

Receiving sensitivity control circuit for radar

Info

Publication number
JPS61202174A
JPS61202174A JP60044328A JP4432885A JPS61202174A JP S61202174 A JPS61202174 A JP S61202174A JP 60044328 A JP60044328 A JP 60044328A JP 4432885 A JP4432885 A JP 4432885A JP S61202174 A JPS61202174 A JP S61202174A
Authority
JP
Japan
Prior art keywords
memory
antenna
elevation
radar
distance
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
JP60044328A
Other languages
Japanese (ja)
Inventor
Suminori Murakami
村上 角憲
Noriyuki Shiraishi
白石 紀之
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.)
NEC Corp
Original Assignee
NEC 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 NEC Corp filed Critical NEC Corp
Priority to JP60044328A priority Critical patent/JPS61202174A/en
Publication of JPS61202174A publication Critical patent/JPS61202174A/en
Pending legal-status Critical Current

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  • Radar Systems Or Details Thereof (AREA)

Abstract

PURPOSE:To perform an automatic control of attenuation level according to the angle of elevation of an antenna, by memorizing a radar received signal attenuation level at in respective zones subdivided in terms of distance and bearing into a memory circuit at each angle of elevation of the antenna. CONSTITUTION:When a memory 13 is accessed with distance and bearing addresses 34 and 35 to supply attenuation level 30 manually inputted while the antenna angle 35 of elevation is specified by an input circuit 10, a radar received signal attenuation level in respective cell zones subdivided in terms of distance and bearing at each antenna angle of elevation is written and memorized into the memory 13. The memory contents thereof are read from the memory 13 according to the antenna angle of elevation using the target bearing and distance from an azimuth address counter 15 and a range address counter 14 as address and outputted via a D/A converter 12 to control the receiving sensitivity. Thus, the automatic attenuation level control of the radar received signal is performed according to the antenna angle of elevation to impart a required attenuation level easily and positively for a higher target/clutter ratio thereby assuring a greater freedom for radar operation.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明はターゲット/クラッタ−比(T/C比:Tar
get  to C1utter Ratio)i改善
した8TC機能を有するレーダの受信感度制御回路に関
する。
DETAILED DESCRIPTION OF THE INVENTION (Industrial Application Field) The present invention is directed to a target/clutter ratio (T/C ratio: Tar
This invention relates to a receiver sensitivity control circuit for a radar having an improved 8TC function.

(従来の技術) 一般に、レーダ装置においては、種々雑多な反射信号の
中から航空機の信号だけを取出すためのクラッタ抑圧技
術・が主要な課顕であり、そのための代表的技術として
移動目標指示(以下MTIという)技術がある。しかし
、このMTI技術だけでは近距離からの強いグランドク
ラツタ上に重畳したターゲットの探知は困難であり、空
中線装置の放射特性を高仰角補正コセカ/ト2乗パター
ン(Modified Co5ecant 8quar
ed Pattern)とし、高仰角の空中線利得を増
加するとともに、この増加利得によりターゲット受信電
力の増加した分に対して一定の減衰量を与えることによ
りT/C比の改善を図っている。
(Prior Art) In general, in radar equipment, the main challenge is clutter suppression technology to extract only aircraft signals from various reflected signals, and a typical technology for this purpose is a moving target indication ( There is a technology (hereinafter referred to as MTI). However, it is difficult to detect targets superimposed on strong ground clutter from a short distance using this MTI technology alone.
The T/C ratio is improved by increasing the antenna gain at high elevation angles and by providing a constant amount of attenuation to the increased target received power due to this increased gain.

この一定の減衰量を与える機能は8TCと呼ばれるが、
この8TC機能を最も有効に発揮させるためには、ター
ゲット受信電力強度とクラッタの受信電力強度および分
布に応じSTC減衰量を変える手段として、レーダ情報
をレンジ(距離)とアジマス(方位)の各々に対して分
割したいくつかのエリア(領域)を設定し、これら各エ
リアに対し距離の4乗、2乗等に反比例した8TC1距
離に関係なく一定の減衰量特性を有するSTC等の組み
合わせによシ最適8TCが与えられる。
This function that provides a certain amount of attenuation is called 8TC,
In order to make the most effective use of this 8TC function, radar information must be divided into range (distance) and azimuth (direction) as a means of changing the STC attenuation according to the target received power strength and clutter received power strength and distribution. For each area, we set up several areas (areas) divided into 8TCs, which are inversely proportional to the 4th power, 2nd power, etc. of the distance. An optimal 8TC is given.

しかし、ターゲット受信電力強度とクラッタ受信電力強
度とは、空中線の設置高度および空中線仰角(空中線ビ
ーム角度)によって変化する。この空中線設置高度は空
中線自体の取付場所(土地および建造物等)によって決
定され容易に変化することはかいが、空中線仰角は自動
もしくは手動により容易に変えられる考慮されている。
However, the target received power intensity and the clutter received power intensity change depending on the installation altitude of the antenna and the antenna elevation angle (the antenna beam angle). Although the antenna installation altitude is determined by the installation location of the antenna itself (land, buildings, etc.) and can easily change, it is considered that the antenna elevation angle can be easily changed automatically or manually.

しかし。but.

この空中線仰角に対応して8TC設定を自動的に行うよ
うに考慮はなされていない。
No consideration is given to automatically setting the 8TC in response to this antenna elevation angle.

第2図(a)はレーダの垂直覆城図の一例である。FIG. 2(a) is an example of a vertical cover diagram of the radar.

図中、垂直覆域1は、ある空中線仰角時の覆域。In the figure, vertical coverage area 1 is the coverage area at a certain antenna elevation angle.

もう一方の垂直覆域2は垂直覆域IK対して仰角が高い
場合の覆域である。なお、一定高度3は地球の湾曲によ
って曲線となっている。この覆域1゜2を有するレーダ
装置における一定高度3のターゲット受信電力強度は、
第2図(1)lに示すように、覆域1に対するターゲッ
ト受信電力4および覆域2に対するターゲット受信電力
5のようになる。
The other vertical coverage area 2 is a coverage area when the elevation angle is higher than the vertical coverage area IK. Note that the constant altitude 3 is a curved line due to the curvature of the earth. The target received power strength at a constant altitude of 3 in this radar device with a coverage area of 1°2 is:
As shown in FIG. 2(1)l, the target received power is 4 for the coverage area 1 and the target received power 5 is for the coverage area 2.

これらのターゲット受信電力に対する最適STC全設定
設定例て、レーダ装置からターゲット迄の距離が変わっ
ても一定のターゲット受信電力強度が得られるのは、第
2図(c)に示すよりな8TC設定となる。図中、8’
rC減衰量6はターゲット受信電力4に対するもの、8
TC減衰量7はターゲット受信電力5に対するものであ
る。これらのSTC減衰量6.7かられかるように空中
線仰角の変化により最適S’l’C設定は変動し、8T
C?最適に設定するためには、8TC減衰量の設定をそ
れぞれの空中線仰角に対応して行なう必要があり、この
ことがレーダ運用中に自由に空中線仰角を変えることに
対する制限と彦る問題があった。
As an example of the optimal STC total settings for these target received power, the 8TC setting shown in Figure 2(c) provides a constant target received power strength even if the distance from the radar device to the target changes. Become. In the figure, 8'
rC attenuation amount 6 is for target received power 4, 8
The TC attenuation amount 7 is for the target received power 5. As can be seen from these STC attenuations of 6.7, the optimum S'l'C setting changes due to changes in the antenna elevation angle, and 8T
C? In order to set it optimally, it is necessary to set the 8TC attenuation in accordance with each antenna elevation angle, which poses a problem that limits the ability to freely change the antenna elevation angle during radar operation. .

(発明の目的) 本発明の目的は、このような問題を解決り、 8TCに
より受信信号に減衰量を与える場合に、空中線仰角に対
応してレンジ方向およびアジマス方向に段階もしくはあ
る関数に従って変化させることにより、レーダ運用の自
由度を拡大したレーダの受信感度制御回路を提供するこ
とにある。
(Object of the Invention) The object of the present invention is to solve such problems, and when attenuating a received signal using 8TC, the range direction and the azimuth direction are changed in steps or according to a certain function in response to the antenna elevation angle. Accordingly, it is an object of the present invention to provide a radar reception sensitivity control circuit that expands the degree of freedom in radar operation.

(発明の構成) 本発明のレーダ受信感度制御回路は、レーダ受信情報を
距離と方位との各々に対して細分化しこれら細分化によ
って決定される区画毎に受信信号減衰量データを記憶す
るメモリ回路と、このメモリ回路へのデータ読込みおよ
びデータ読出しを切替えるスイッチ回路と、前記メモリ
回路へ減衰量データを読込ませるデータ入力回路と、前
記メモリ回路に記憶された減衰量データをレーダ受信信
号の距離および方位および空中線仰角に対応させて読出
しレーダ受信感度を制御する減衰量読出回路とを含み構
成される。
(Structure of the Invention) The radar reception sensitivity control circuit of the present invention is a memory circuit that subdivides radar reception information into distance and direction and stores received signal attenuation amount data for each section determined by these subdivisions. a switch circuit that switches between reading and reading data into the memory circuit; a data input circuit that reads attenuation data into the memory circuit; The attenuation amount readout circuit controls the readout radar reception sensitivity in correspondence with the azimuth and the antenna elevation angle.

(賽施例) 次に本発明を図面により詳細に説明する。(Saving example) Next, the present invention will be explained in detail with reference to the drawings.

第1図は本発明の一実施例のブロック図である。FIG. 1 is a block diagram of one embodiment of the present invention.

図において、10は距離(レンジ)および方位(アジマ
ス)および空中線仰角に対応して減衰量を設定するデー
タ入力回路、11.14はラッチ回路、12はD/A変
換器、13はメモリ、15は入力端子21.22からの
方位角基準信号(AR,P)およびインクリメンタルパ
ルス信号(ACP)とによりアジマスを読出すアジマス
アドレスカウンタ、16は入力端子23.24からのO
レンジトリガおよびクロックに従がってレンジを読み出
すレンジアジマスカウンタ、81〜S4はメモリ13ヘ
データ入力を行う時と読出時とを切替えるスイッチであ
る。
In the figure, 10 is a data input circuit that sets the amount of attenuation in accordance with the distance (range), azimuth, and antenna elevation angle, 11.14 is a latch circuit, 12 is a D/A converter, 13 is memory, and 15 16 is an azimuth address counter that reads out the azimuth using the azimuth reference signal (AR, P) and the incremental pulse signal (ACP) from input terminals 21.22, and 16 is O from input terminal 23.24.
Range azimuth counters 81 to S4 that read the range according to the range trigger and the clock are switches that switch between inputting and reading data to the memory 13.

まず、データ入力回路10にデータ全入力する場合、ス
イッチ81〜84をデータ入力側に設定してアジマスア
ドレス信号33.レンジアドレス信号34および空中線
仰角信号35を指定し、メモリ制御信号(CONT)3
2に従がって減衰量入力データが設定される。
First, when inputting all data to the data input circuit 10, the switches 81 to 84 are set to the data input side and the azimuth address signal 33. Specifies the range address signal 34 and antenna elevation angle signal 35, and outputs the memory control signal (CONT) 3.
Attenuation amount input data is set according to 2.

この場合の減衰量入力設定は、第3図(alおよび(b
)、第4図(alおよび中)のように行われる。すなわ
ち、STC減衰減衰量デカデータ30レーダ情報をレン
ジとアジマスの各々に対して細分化し、この細分化によ
って決定されるセルごとにデータ入力回路10により手
動にて設定されメモリ13に入力される。この場合、第
3図(a)、 (b)のように、レンジとアジマスの細
分化により生じる区画がセルからなり、各セル内の数字
が減衰量データの一例を示し、また第4図(a)、 (
b)ではこの設定例を3次元的に表示したものである。
The attenuation input settings in this case are shown in Figure 3 (al and (b)
), as shown in Figure 4 (al and middle). That is, the STC attenuation deca data 30 radar information is subdivided into range and azimuth, and each cell determined by this subdivision is manually set by the data input circuit 10 and input into the memory 13. In this case, as shown in FIGS. 3(a) and 3(b), the divisions resulting from subdivision of range and azimuth are made up of cells, and the numbers in each cell indicate an example of attenuation data, and as shown in FIG. a), (
In b), this setting example is displayed three-dimensionally.

次に、設定された減衰量データを使用するためにメモリ
13から減衰量データを読出す場合、まずスイッチ81
〜S4が読出例(使用時)に切替えられる。この時の動
作タイミングは第5図(a)〜(e)の波形図に示され
る。
Next, when reading the attenuation amount data from the memory 13 in order to use the set attenuation amount data, first switch 81
~S4 is switched to the reading example (when used). The operation timing at this time is shown in the waveform diagrams of FIGS. 5(a) to 5(e).

第1図において、メモリ13に入力された減衰量データ
30はレンジ0の位置に発生するゼロレンジトリガ(第
5図(a))とクロック信号および空中線の特定回転方
向から得られる方位角基準信号(ARP)とインクリメ
ンタルパルス信号(ACP)をそれぞれ入力端子23.
24,22.21から受け、レンジアジマスカウンタ1
5とアジマスアドレスカウンタ16および空中線仰角信
号によりアドレスを指定してメモリ内容の読み出しが行
なわれる。このレンジアドレスカウンタ16の出力は、
第5図(b)のように5例えばレンジ0から最大200
 浬まで順次読出しが行われる。また、アジマスアドレ
スカウンタ15の出力は、第5図(c)のように、例え
ば10’、10.1°のようにアドレス指定が行われる
。このアジマスアドレスカウンタ15により得られた方
位情報は、0レンジトリガごとにラッチ回路14により
ラッチされる。空中線仰角信号は第5図(d)のように
例えば2°のようにアドレス指定が行われる。これらの
各アドレス情報によってメモリ内容の減衰量データ(第
5図(e))の読み出し金行う。
In FIG. 1, attenuation amount data 30 input to the memory 13 are a zero range trigger (FIG. 5(a)) generated at the position of range 0, a clock signal, and an azimuth reference signal obtained from a specific rotational direction of the antenna. (ARP) and incremental pulse signal (ACP) at input terminals 23.
24, 22. Received from 21, range azimuth counter 1
5, an azimuth address counter 16, and an antenna elevation angle signal to designate an address and read out the memory contents. The output of this range address counter 16 is
For example, range 0 to maximum 200 as shown in Figure 5(b).
Reading is performed sequentially until the end. Further, the output of the azimuth address counter 15 is addressed, for example, as 10' and 10.1°, as shown in FIG. 5(c). The azimuth information obtained by the azimuth address counter 15 is latched by the latch circuit 14 for each 0 range trigger. The antenna elevation angle signal is addressed, for example, by 2°, as shown in FIG. 5(d). The attenuation amount data (FIG. 5(e)) of the memory contents is read based on each of these address information.

この読み出された減衰量データ信号31は、ラッチ回路
11でラッチされた後D/Afi換器12を経由して出
力端子20から8TC回路の駆動用信号として出力され
る。
The read attenuation amount data signal 31 is latched by the latch circuit 11 and then outputted from the output terminal 20 as a drive signal for the 8TC circuit via the D/Afi converter 12.

(発明の効果) 以上説明したように、本発明によれば、空中線仰角に対
応して8TC減衰量を変化させることが可能となり、レ
ーダ運用中に空中線仰角を変えた場合その都度8TCの
設定変更全手動によって行なわないですむことになり、
従ってレーダ運用の自由度を拡大する効果を有する。
(Effects of the Invention) As explained above, according to the present invention, it is possible to change the 8TC attenuation amount in accordance with the antenna elevation angle, and the 8TC setting is changed each time the antenna elevation angle is changed during radar operation. This eliminates the need to do everything manually,
Therefore, it has the effect of expanding the degree of freedom in radar operation.

【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(a)
はレーダ垂直覆域図の一例、第2図中)は一定高度3で
のターゲット受信電力強度図、第2図(C)はターゲッ
ト受信電力を一定とするための8TC設定図、第3図(
a)、 (b)、第、4図(a)、 (b)は本実施例
によるSTC減衰量入力データの一例をアジマス。 レンジ、空中線仰角に対応して2次元的および3次元的
に示した特性図、第5図(a)〜(e)は第1図の動作
を説明する波形図である。図において1.2・・・・・
・ある角度の垂直覆域、3・・・・・・一定高度、4.
5・・・・・・一定高度3におけるターゲット受信強度
、6,7・・・・・・STC減衰量、10・・・・・・
データ入力回路、11.14・・・・・・ラッチ回路、
12・・・・・・D/A変換器、13・・・・・・メモ
リ、15・・・・・・アジマスアドレスカウンタ、16
・・・・・・レンジアドレスカウンタ、20・・・・・
・STC回路駆動信号出力端子、21・・・・・・AC
P入力端子、22・・・・・・ARP入力端子、23・
・・・・・0レンジトリガ入力端子、24・・・・・・
クロック入力端子、25・・・・・・空中線仰角入力端
子、30・・・・・・STC減衰減衰量デカデータ1・
・・・・・読み出されたSTC減衰量データ、32・・
・・・・メモリ制御信号、33・・・・・・アジマスア
トt/ス信号、34・・・・・・レンジアドレス信号、
35・・・・・・空中線仰角信号である。 −一シ;ソ 茅2已 二1フ17−    (レノ
[Brief Description of the Drawings] Figure 1 is a block diagram of an embodiment of the present invention, Figure 2 (a)
is an example of a radar vertical coverage map, Figure 2 (in Figure 2) is a target received power intensity diagram at a constant altitude of 3, Figure 2 (C) is an 8TC setting diagram to keep the target received power constant, Figure 3 (
Figures 4 (a) and 4 (b) show examples of STC attenuation input data according to this embodiment in azimuth. Characteristic diagrams shown two-dimensionally and three-dimensionally in correspondence to the range and the antenna elevation angle, and FIGS. 5(a) to 5(e) are waveform diagrams illustrating the operation of FIG. 1. In the figure 1.2...
・Vertical coverage area at a certain angle, 3... constant altitude, 4.
5...Target reception strength at constant altitude 3, 6,7...STC attenuation, 10...
Data input circuit, 11.14...Latch circuit,
12...D/A converter, 13...Memory, 15...Azimuth address counter, 16
...Range address counter, 20...
・STC circuit drive signal output terminal, 21...AC
P input terminal, 22...ARP input terminal, 23.
...0 range trigger input terminal, 24...
Clock input terminal, 25... Antenna elevation angle input terminal, 30... STC attenuation attenuation deca data 1.
...Read out STC attenuation data, 32...
...Memory control signal, 33...Azimuth at/s signal, 34...Range address signal,
35...Antenna elevation angle signal. -1shi; Somo2 21fu 17- (Reno

Claims (1)

【特許請求の範囲】[Claims] レーダ受信情報を距離と方位との各々に対して細分化し
これら細分化によって決定される区画毎に受信信号減衰
量データを記憶するメモリ回路と、このメモリ回路への
データ読込みおよびデータ読出しを切替えるスイッチ回
路と、前記メモリ回路への減衰量データを読込ませるデ
ータ入力回路と、前記メモリ回路に記憶された減衰量デ
ータをレーダ受信信号の距離、方位および空中線仰角に
対応させて読出しレーダ受信感度を制御する減衰量読出
回路とを含むレーダの受信感度制御回路。
A memory circuit that subdivides radar reception information into each of distance and direction and stores received signal attenuation data for each section determined by these subdivisions, and a switch that switches between reading data into and reading out data from this memory circuit. a data input circuit for reading attenuation data into the memory circuit; and a data input circuit for reading attenuation data stored in the memory circuit in correspondence with the distance, azimuth, and antenna elevation angle of a radar reception signal to control radar reception sensitivity. A radar reception sensitivity control circuit including an attenuation amount readout circuit.
JP60044328A 1985-03-06 1985-03-06 Receiving sensitivity control circuit for radar Pending JPS61202174A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60044328A JPS61202174A (en) 1985-03-06 1985-03-06 Receiving sensitivity control circuit for radar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60044328A JPS61202174A (en) 1985-03-06 1985-03-06 Receiving sensitivity control circuit for radar

Publications (1)

Publication Number Publication Date
JPS61202174A true JPS61202174A (en) 1986-09-06

Family

ID=12688436

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60044328A Pending JPS61202174A (en) 1985-03-06 1985-03-06 Receiving sensitivity control circuit for radar

Country Status (1)

Country Link
JP (1) JPS61202174A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04157385A (en) * 1990-10-19 1992-05-29 Nec Corp Stc system of radar
JPH04318484A (en) * 1991-04-17 1992-11-10 Furuno Electric Co Ltd Radar receiver
JPH04318483A (en) * 1991-04-17 1992-11-10 Furuno Electric Co Ltd Radar receiver
JPH04318482A (en) * 1991-04-17 1992-11-10 Furuno Electric Co Ltd Radar receiver
JPH07167943A (en) * 1993-12-15 1995-07-04 Nec Corp Radar device
JP2008185357A (en) * 2007-01-26 2008-08-14 Toshiba Corp Radar signal processing apparatus

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5883285A (en) * 1981-11-12 1983-05-19 Mitsubishi Electric Corp Radar device
JPS5944591A (en) * 1982-09-03 1984-03-13 Nissan Motor Co Ltd Rotary type regenerative heat exchanger

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5883285A (en) * 1981-11-12 1983-05-19 Mitsubishi Electric Corp Radar device
JPS5944591A (en) * 1982-09-03 1984-03-13 Nissan Motor Co Ltd Rotary type regenerative heat exchanger

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04157385A (en) * 1990-10-19 1992-05-29 Nec Corp Stc system of radar
JPH04318484A (en) * 1991-04-17 1992-11-10 Furuno Electric Co Ltd Radar receiver
JPH04318483A (en) * 1991-04-17 1992-11-10 Furuno Electric Co Ltd Radar receiver
JPH04318482A (en) * 1991-04-17 1992-11-10 Furuno Electric Co Ltd Radar receiver
JPH07167943A (en) * 1993-12-15 1995-07-04 Nec Corp Radar device
JP2008185357A (en) * 2007-01-26 2008-08-14 Toshiba Corp Radar signal processing apparatus

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