JPH0196575A - Radar signal simulating device - Google Patents

Radar signal simulating device

Info

Publication number
JPH0196575A
JPH0196575A JP25411387A JP25411387A JPH0196575A JP H0196575 A JPH0196575 A JP H0196575A JP 25411387 A JP25411387 A JP 25411387A JP 25411387 A JP25411387 A JP 25411387A JP H0196575 A JPH0196575 A JP H0196575A
Authority
JP
Japan
Prior art keywords
signal
distance
clutter
azimuth
gate
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
JP25411387A
Other languages
Japanese (ja)
Inventor
Chiaki Matsui
松井 千明
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric 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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP25411387A priority Critical patent/JPH0196575A/en
Publication of JPH0196575A publication Critical patent/JPH0196575A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To raise an operator's attending sense by adding an interpolation arithmetic part for executing a high speed interpolation processing by a hardware, between an azimuth distance memory and a comparator. CONSTITUTION:By a control use computer 1, a clutter generating range is determined and sent out to an azimuth distance memory 4. The memory 4 outputs distance signals R1(B), R2(B) to interpolation arithmetic parts 5a, 5b. The arithmetic parts 5a, 5b executes an interpolation processing by bringing the present input signal to proportional distribution into equal parts. A distance interpolating signal as a result of interpolation processing is outputted synchronously with a trigger signal. This distance interpolating signal is compared with a reference distance signal of a distance counter 6 by comparators 7a, 7b, and a gate control use pulse is generated. By this pulse, a gate signal is generated by a gate generating circuit 9, and in a gate 11, only a necessary part of an attenuation characteristic signal is fetched and a modulating signal is generated. A clutter original signal which has been modulated by the modulating signal becomes a clutter signal, displayed on a radar indicating machine 13 and becomes a clutter echo being similar to a clutter shape in an actual radar.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、捜索レーダのレーダ指示機操作員のための
訓練に用いるレーダの模擬信号を発生する装置のうちク
ラッタ発生方法に関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a method for generating clutter in a device for generating a simulated radar signal used for training radar indicating machine operators of a search radar.

〔従来の技術〕[Conventional technology]

第5図は従来のレーダ信号模擬装置のクラッタ発生制御
部のブロック図であシ、(1)はクラッタの発生範囲を
制御する制御用計算機、(2)は実レーダの送信タイミ
ング及び空中線の回転を模擬するタイミング発生回路、
(3)は空中線方位角をメモリのアドレスに変換する方
位カウンタ、(4)は上記空中線方位角に対応させクラ
ッタ発生範囲を距離情報として記憶する方位距離メモリ
、(6)は上記タイミング発生回路に同期して基準距離
信号を発生する距離カウンタ、(7a) 、 (7b)
は、上記方位距離メモリの距離信号出力と上記距離カウ
ンタの基準距離信号出力とを比較して両者が一致した時
にパルスを出力fるコンパレータ、(8)はクラッタの
距離による強度変化を模擬するだめの減衰特性制御部で
ある。第6図は同じ〈従来のレーダ信号模擬装置のクラ
ッタ発生変調部及びレーダ指示機のブロック図でちり(
9)は上記コンパレータ出力パルスによりクラッタ存在
範囲のみにゲート信号を発生させるゲート発生回路、 
+11はクラッタのからのレーダ電波の反射を模擬する
原信号を発生するクラッタ原信号発生器、Uは上記ゲー
ト発生回路のゲート信号出力により上記減衰特性制御部
の減衰特性信号をゲーティングするグー)、aX5はク
ラッタ原信号を振幅変調する変調回路、(I3はレーダ
指示機である。第7図は従来のレーダ信号模擬装置で発
生したクラッタのレーダ指示機上の表示の一例を示した
イメージ図で(41b)はクラッタエコーである。
Figure 5 is a block diagram of the clutter generation control section of a conventional radar signal simulator, in which (1) is a control computer that controls the clutter generation range, and (2) is the actual radar transmission timing and antenna rotation. A timing generation circuit that simulates
(3) is an azimuth counter that converts the antenna azimuth into a memory address; (4) is an azimuth/distance memory that stores the clutter occurrence range as distance information in correspondence with the antenna azimuth; and (6) is the timing generation circuit. Distance counters that synchronously generate reference distance signals, (7a), (7b)
(8) is a comparator that compares the distance signal output of the azimuth and distance memory with the reference distance signal output of the distance counter and outputs a pulse when the two match; This is the damping characteristic control section. Figure 6 is the same block diagram of the clutter generation modulator and radar indicator of the conventional radar signal simulator.
9) is a gate generation circuit that generates a gate signal only in the clutter existing range using the comparator output pulse;
+11 is a clutter original signal generator that generates an original signal that simulates the reflection of radar radio waves from clutter, and U is a gate signal generator that gates the attenuation characteristic signal of the attenuation characteristic control section using the gate signal output of the gate generation circuit. , aX5 is a modulation circuit that amplitude modulates the clutter original signal, (I3 is a radar indicator. Fig. 7 is an image diagram showing an example of the display of clutter on the radar indicator that occurs in a conventional radar signal simulator. (41b) is a clutter echo.

次に動作について説明する。制御用計算機+11ではク
ラッタを発生させようとする範囲を空中線の方位角に従
って奄近端距離R1(B)、i遠端距離R2(B)の極
座棟系式で方位距離メモリ(4)に送出し記憶させる。
Next, the operation will be explained. In the control computer +11, the range in which clutter is to be generated is stored in the azimuth distance memory (4) according to the azimuth angle of the antenna using a polar base system formula of near end distance R1 (B) and i far end distance R2 (B). Send and store.

タイミング発生回路(2)では模擬しようとしている実
レーダの空中線の回転速度と同一の変化率で方位角信号
を発生し方位カウンタ(3)に出力し、方位距離メモリ
(4)に記憶した距離信号It+(B)及びR2(B)
  を読み出す。タイミング発生回路(2)では同時に
トリガ信号R,を発生し、距離カウンタ(6)をこのト
リガ信号に同期させて動作させ基準距離信号を発生する
。コンパレータ(7a) 。
The timing generation circuit (2) generates an azimuth signal at the same rate of change as the rotation speed of the antenna of the actual radar to be simulated, outputs it to the azimuth counter (3), and generates a distance signal stored in the azimuth and distance memory (4). It+(B) and R2(B)
Read out. The timing generating circuit (2) simultaneously generates a trigger signal R, and operates a distance counter (6) in synchronization with this trigger signal to generate a reference distance signal. Comparator (7a).

(7b)では上記方位距離メモ月4)の距離信号出力と
(7b) is the distance signal output of the above azimuth distance memo month 4).

上記距離カウンタ(6)の基準距離信号とを比較し。Compare with the reference distance signal of the distance counter (6).

一致した時にパルスを発生する。ゲート発生回路(9)
は上記パルスを入力しR1(B)からR2(B)  ま
での間ゲート信号を発生させる。減衰特性制御部(8)
では上記距離カウンタ(6)の基準距離信号により減衰
特性信号を出力し、この減衰特性信号はゲートαυにお
いて上記ゲート発生回路(9)のゲート信号によりゲー
ティングされ最終変調信号が得られる。この変調信号に
よりクラッタ原信号発生器αQの出力を変調回路α2に
て振幅変調し、クラッタ信号を得る。クラッタ信号はレ
ーダ指示機a3の電子管上に空中線方位角B及びトリガ
信号ROに同期して表示されクラッタイメージ(41b
)として表われる。
Generates a pulse when a match occurs. Gate generation circuit (9)
inputs the above pulse and generates a gate signal from R1(B) to R2(B). Attenuation characteristic control section (8)
Then, an attenuation characteristic signal is output based on the reference distance signal of the distance counter (6), and this attenuation characteristic signal is gated by the gate signal of the gate generation circuit (9) at the gate αυ to obtain a final modulation signal. Using this modulation signal, the output of the clutter original signal generator αQ is amplitude-modulated in the modulation circuit α2 to obtain a clutter signal. The clutter signal is displayed on the electron tube of the radar indicator a3 in synchronization with the antenna azimuth B and the trigger signal RO, and the clutter image (41b
).

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

従来のレーダ信号模擬装置は以上のように構成されてい
るのでレーダ指示機上のクラッタ形状は方位角の分解能
によるところが多く制御用計算機の処理速度及び方位距
離メモリの容量の制限から分解能を高く出来ずクラッタ
形状が扇形となってしまい、実レーダのクラッタとは似
つかないものとなり、操作員の訓練に用いるには不十分
であった。
Since the conventional radar signal simulator is configured as described above, the shape of clutter on the radar indicator largely depends on the azimuth resolution, and it is difficult to increase the resolution due to limitations in the processing speed of the control computer and the capacity of the azimuth and distance memory. However, the clutter was fan-shaped and did not resemble the clutter of an actual radar, making it unsuitable for use in operator training.

この発明は上記のような問題点を解消するためになされ
たもので、レーダ指示機上に表われるクラッタ形状をよ
り実レーダに近づけ操作員の臨場感を高めることができ
るレーダ信号模擬装置を得ることを目的とする。
This invention was made to solve the above-mentioned problems, and provides a radar signal simulating device that can bring the clutter shape appearing on the radar indicator closer to the actual radar and enhance the operator's sense of reality. The purpose is to

〔問題点を解決するための手段〕[Means for solving problems]

この発明に係るレーダ信号模擬装置は制御用計算機の処
理速度及び方位距離メモリの容量を変更することなしに
クラッタ形状の方位分解能を向上させるために方位距離
メモリとコンパレータの間にハードウェアで高速補間処
理を行う補間演算部を付加したものである。
The radar signal simulator according to the present invention uses hardware to perform high-speed interpolation between the azimuth and distance memory and the comparator in order to improve the azimuth resolution of the clutter shape without changing the processing speed of the control computer or the capacity of the azimuth and distance memory. It has an additional interpolation calculation section that performs processing.

〔作用J この発明における補間演算部は方位距離メモリにおける
ある方位Bi の距離信号R1(Bt)。
[Operation J] The interpolation calculation unit in this invention calculates the distance signal R1 (Bt) of a certain direction Bi in the direction and distance memory.

R2(B i )と次の方位13i+1の距離信号R1
(J+1) 。
R2 (B i ) and the distance signal R1 of the next direction 13i+1
(J+1).

R2(Bi−H)の閂をそれぞれ等分に比例補間するも
のであり1等価的に方位分解能を向上することとなる。
The R2 (Bi-H) bolts are proportionally interpolated into equal parts, and the azimuth resolution is improved by one equivalent.

〔実施例〕〔Example〕

以下、この発明の一実施例を図について説明する。 An embodiment of the present invention will be described below with reference to the drawings.

第1図において(1)は制御用計算機、(2)はタイミ
ング発生回路(3)は方位カウンタ、(4)は方位距離
メモリ、  (5a)、(5b)は方位距離メモリの距
離信号を補間処理する補間演算部、(6)は距離カウン
タ。
In Figure 1, (1) is a control computer, (2) is a timing generation circuit, (3) is an azimuth counter, (4) is an azimuth distance memory, and (5a) and (5b) are interpolated distance signals from the azimuth and distance memory. The processing interpolation calculation unit (6) is a distance counter.

(7a) 、 (7b)はコンパレータ、(8)は減衰
特性制御部である。第2図において(9)はゲート発生
回路、 IIGはクラッタ原信号発生器、αυはゲート
、 (13は変調回路、 (131はレーダ指示機であ
る。第3図はこの発明の一実施例における各部の信号の
タイミングを示したタイミング図でちり1図において0
11はトリガ信号0国は距離信号の読み出しタイミング
(7a) and (7b) are comparators, and (8) is an attenuation characteristic control section. In FIG. 2, (9) is a gate generation circuit, IIG is a clutter original signal generator, αυ is a gate, (13 is a modulation circuit, and (131 is a radar indicator). This is a timing diagram showing the signal timing of each part.
11 is the trigger signal 0 country is the read timing of the distance signal.

(35a) 、 (35b)は距離補間信号の出力タイ
ミング。
(35a) and (35b) are the output timings of the distance interpolation signal.

(34a) 、 (34b)はゲート制御用のコンパレ
ータ出力パルス、@はゲート信号、(至)は減衰特性信
号、@は変調信号、(至)はクラッタ原信号、 01は
クラッタ信号である。第4図はこの発明のマ実施例にお
けるレーダ指示機上のクラッタ表示を示すイメージ図で
(41a)はクラッタエコーである。
(34a) and (34b) are comparator output pulses for gate control, @ is a gate signal, (to) is an attenuation characteristic signal, @ is a modulation signal, (to) is a clutter original signal, and 01 is a clutter signal. FIG. 4 is an image diagram showing the clutter display on the radar indicator in the embodiment of the present invention, and (41a) is a clutter echo.

この発明は以上のようになっているから、制御用計算機
(1)にてクラッタ発生範囲を決定し方位距離メモリに
送出するまでの動作は従来のレーダ信号模擬装置と同様
でちるが、距離信号の読み出しタイミング(2)はトリ
ガ信号の周期の整数倍(実施例では説明の都合上4倍と
した)に同期して行われ、かつ方位カウンタ(3)では
レーダ指示機に出力される万位角Bi に対しB!+1
 の進んだアドレスを方位距離メモリ(4)に指定する
。方位距離メモリ(4)は距離信号R1(J−H)、 
 R2(B++、)  を上記タイミングで補間演算部
(5a)、 (5b)に出力する。補間演算部では前入
力距離信号R1(J)、 R2(Bi)をレジスタに入
力しておき現在の入力信号R+ (B H−1) 、 
R2(B i−H)との間を等分に比例配分することに
より補間処理を行う。補間された結果の距離補間信号は
トリガ信号0σに同期して、 (33a)(55b’)
に示すタイミングで出力される。距離補間信号は距離カ
ウンタ(6)の基準距離信号とコンパレータ(7a) 
、 (7b)で比較され、ゲート制御用パルス(34a
) 、 (34b)が発生する。このパルスによりゲー
ト信号(至)がゲート発生口m+91で作られゲー)(
Lllにおいて減衰特性2号(1)の必要部分のみ取り
出し変調信号0ηが発生する。変調信号(ロ)で変調さ
れたクラック原信号(至)はクラッタ信号(至)となフ
レーダ指示機03上に表示され実レーダにおけるクラッ
タ形状に近いクラッタエコー(41a) トl ル。
Since the present invention is configured as described above, the operation from determining the clutter occurrence range to the azimuth and distance memory in the control computer (1) is the same as that of the conventional radar signal simulating device, but the distance signal The reading timing (2) is performed in synchronization with an integral multiple of the period of the trigger signal (in the example, it is set to 4 times for convenience of explanation), and the direction counter (3) outputs the ten-man direction to the radar indicator. B for angle Bi! +1
The advanced address is specified in the azimuth and distance memory (4). The azimuth distance memory (4) contains the distance signal R1 (J-H),
R2(B++,) is output to the interpolation calculation units (5a) and (5b) at the above timing. In the interpolation calculation section, the previous input distance signals R1 (J) and R2 (Bi) are input into registers, and the current input signals R+ (B H-1),
Interpolation processing is performed by equally proportionally allocating between R2 (B i-H). The interpolated distance interpolation signal is synchronized with the trigger signal 0σ, (33a) (55b')
It is output at the timing shown in . The distance interpolation signal is the reference distance signal of the distance counter (6) and the comparator (7a).
, (7b) and the gate control pulse (34a
), (34b) occur. This pulse generates a gate signal (to) at the gate generation port m+91.
At Lll, only the necessary portion of the attenuation characteristic No. 2 (1) is taken out and a modulated signal 0η is generated. The crack original signal (to) modulated by the modulation signal (b) is displayed on the radar indicator 03 as a clutter signal (to), and is a clutter echo (41a) close to the clutter shape in the actual radar.

なお、説明の都合上、上期実施例では、距離補間の数を
4.出力タイミングをトリガ信号周期と同一としたが、
出力タイミングはトリガ信号の整数倍であればいくつで
もよく、同様に距離補間の数も整数であればよく、上記
実施例と同様の効果を奏する。
For convenience of explanation, in the first embodiment, the number of distance interpolations is set to 4. The output timing was set to be the same as the trigger signal period, but
The output timing may be any number as long as it is an integer multiple of the trigger signal, and similarly the number of distance interpolations may be an integer, producing the same effects as in the above embodiment.

〔発明の効果〕〔Effect of the invention〕

以上のように、この発明によれば、補間演算部を付加し
たため、制御用計算機または方位距離メモリ等装置全体
に影響する仕様を変更することなしにより実レーダにお
けるクラッタ形状に近いクラッタ模擬信号を得ることが
でき、し−ダ指示機操作員の訓練を行うためのレーダ信
号模擬装置として高い臨場感が得られる効果がある。
As described above, according to the present invention, since the interpolation calculation unit is added, a clutter simulation signal close to the clutter shape in an actual radar can be obtained without changing the specifications that affect the entire device, such as the control computer or azimuth distance memory. It has the effect of providing a high sense of realism as a radar signal simulating device for training radar indicating machine operators.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図及び第2図はこの発明の一実施例を示すブロック
図、第3図はこの発明の一実施例における動作タイミン
グを示すタイミング図、第4図はこの発明の一実施例に
おける信号表示例を示すイメージ図、第5図及び第6図
は従来のレーダ信号模擬装置のブロック図、第1図は従
来のレーダ信号模擬装置における信号表示例を示すイメ
ージ図である。 図において、(1)は制御用計算機、 (21fiタイ
ミング発生回路、(3)は方位カウンタ、(4)は方位
距離メモリ、  (sa)、 (5b)は補間演算部、
(6)は距離カウンタ、  (7g)、(7b)はコン
パレータ、CB)は減衰特性制御部、(9)はゲート発
生回路、αlはクラッタ原信号発生器、09はゲート、
α2は変調回路、 113はレーダ指示機、C3υはト
リガ信号、oa/ri距離信号読みrB Lタイミング
、  (33a) 、 (33b)は距離補間信号出力
タイミンf、  (5431)、 (54b)はフンパ
レータ出力パルス、(至)はゲート信号、0[9は減衰
特性信号、0乃は変調信号、(至)はクラッタ原信号、
(至)はクラッタ信号。 (41a) 、 (41b)はクラッタエコーである。 なお1図中同一あるいは相当部分には同一符号を付して
示しである。 第2図 M4図 第 6 図 B 第7図
1 and 2 are block diagrams showing one embodiment of this invention, FIG. 3 is a timing diagram showing operation timing in one embodiment of this invention, and FIG. 4 is a signal table in one embodiment of this invention. FIGS. 5 and 6 are block diagrams of a conventional radar signal simulator, and FIG. 1 is an image diagram illustrating an example of a signal display in the conventional radar signal simulator. In the figure, (1) is a control computer, (21fi timing generation circuit), (3) is an azimuth counter, (4) is an azimuth distance memory, (sa), (5b) is an interpolation calculation unit,
(6) is a distance counter, (7g) and (7b) are comparators, CB) is an attenuation characteristic control section, (9) is a gate generation circuit, αl is a clutter original signal generator, 09 is a gate,
α2 is a modulation circuit, 113 is a radar indicator, C3υ is a trigger signal, oa/ri distance signal reading rB L timing, (33a), (33b) are distance interpolation signal output timing f, (5431), (54b) are hump parators Output pulse, (to) is gate signal, 0 [9 is attenuation characteristic signal, 0 to modulation signal, (to) is clutter original signal,
(to) is the clutter signal. (41a) and (41b) are clutter echoes. Note that in FIG. 1, the same or corresponding parts are designated by the same reference numerals. Figure 2 M4 Figure 6 Figure B Figure 7

Claims (1)

【特許請求の範囲】[Claims] クラツタの発生範囲を極座標にて発生し出力する制御用
計算機と、模擬しようとするレーダと同等のトリガ信号
及び空中線の方位角を発生するタイミング発生回路と、
上記タイミング発生回路の方位角をメモリアドレスに変
換する方位カウンタと、上記制御用計算機出力を記憶し
上記方位カウンタの指示によりクラツタ発生範囲の最近
、最速2つの距離信号を送出する方位距離メモリと、上
記方位距離メモリの距離信号を一時的に記憶しかつ比例
配分により補間処理を行う2つの補間演算部と、上記タ
イミング発生回路のトリガ信号出力に同期して基準距離
信号を発生する距離カウンタと、上記基準距離信号と上
記補間演算部の距離補間信号を比較し、一致した時にパ
ルスを出力する2つのコンパレータと、上記基準距離信
号に同期してクラツタの減衰特性を模擬する減衰特性信
号を出力する減衰特性制御部と、上記コンパレータ出力
パルスによりゲート信号を発生するゲート発生回路と、
クラツタ原信号発生器と、上記ゲート信号により上記減
衰特性信号の必要部分のみ取り出し変調信号を発生する
ゲートと上記クラツタ原信号発生器出力信号を上記変調
信号により振幅変調する変調回路とレーダ指示器とを備
えたレーダ信号模擬装置。
A control computer that generates and outputs the range of clutter occurrence in polar coordinates, a timing generation circuit that generates a trigger signal equivalent to that of the radar to be simulated, and an azimuth of the antenna;
an azimuth counter that converts the azimuth of the timing generation circuit into a memory address; an azimuth-distance memory that stores the output of the control computer and sends out the two fastest distance signals recently in the clutter occurrence range according to instructions from the azimuth counter; two interpolation calculation units that temporarily store the distance signal in the azimuth and distance memory and perform interpolation processing by proportional allocation; and a distance counter that generates a reference distance signal in synchronization with the trigger signal output of the timing generation circuit; Two comparators that compare the reference distance signal and the distance interpolation signal of the interpolation calculation unit and output a pulse when they match, and output an attenuation characteristic signal that simulates the attenuation characteristic of clutter in synchronization with the reference distance signal. an attenuation characteristic control section; a gate generation circuit that generates a gate signal using the comparator output pulse;
a Clutter original signal generator, a gate for extracting only a necessary portion of the attenuation characteristic signal using the gate signal and generating a modulation signal, a modulation circuit for amplitude modulating the output signal of the Clutter original signal generator using the modulation signal, and a radar indicator. A radar signal simulator equipped with
JP25411387A 1987-10-08 1987-10-08 Radar signal simulating device Pending JPH0196575A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25411387A JPH0196575A (en) 1987-10-08 1987-10-08 Radar signal simulating device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25411387A JPH0196575A (en) 1987-10-08 1987-10-08 Radar signal simulating device

Publications (1)

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JPH0196575A true JPH0196575A (en) 1989-04-14

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Family Applications (1)

Application Number Title Priority Date Filing Date
JP25411387A Pending JPH0196575A (en) 1987-10-08 1987-10-08 Radar signal simulating device

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Country Link
JP (1) JPH0196575A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0572320A (en) * 1991-05-28 1993-03-26 Nec Corp Pseudo-signal generation device
KR100743021B1 (en) * 2001-04-25 2007-07-27 국방과학연구소 Method of imitation experiment of radar system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0572320A (en) * 1991-05-28 1993-03-26 Nec Corp Pseudo-signal generation device
KR100743021B1 (en) * 2001-04-25 2007-07-27 국방과학연구소 Method of imitation experiment of radar system

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