JPH04194A - Air-to-air fight training supporting apparatus - Google Patents

Air-to-air fight training supporting apparatus

Info

Publication number
JPH04194A
JPH04194A JP9806290A JP9806290A JPH04194A JP H04194 A JPH04194 A JP H04194A JP 9806290 A JP9806290 A JP 9806290A JP 9806290 A JP9806290 A JP 9806290A JP H04194 A JPH04194 A JP H04194A
Authority
JP
Japan
Prior art keywords
signal
radar
aircraft
target
fighter
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
JP9806290A
Other languages
Japanese (ja)
Inventor
Kenji Horiuchi
堀内 健志
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 JP9806290A priority Critical patent/JPH04194A/en
Publication of JPH04194A publication Critical patent/JPH04194A/en
Pending legal-status Critical Current

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Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 [産業上の利用分野コ この発明は1戦闘機パイロットが戦闘機を用いた空対空
戦闘訓練において使用し、空対空戦闘訓練の支援を行う
空対空戦闘訓練支援装置に関するものである。
[Detailed Description of the Invention] [Industrial Application Field] This invention relates to an air-to-air combat training support device that is used by a fighter pilot in air-to-air combat training using a fighter jet and supports the air-to-air combat training. It is something.

[従来の技術] 従来の戦闘機には、空対空戦闘訓練の支援を行うための
攻撃成果を判定する機能を付加したものはなく、空対空
戦闘訓練を行うためには地上に設けられたレーダもしく
は戦闘訓練を行う航空機から送信される電波を受信して
航空機の位置を標定する地上の無線位置標定装置により
戦闘訓練を行っている航空機の相対位置を測定し、攻撃
成果の判定等を行うことにより、空対空戦闘訓練を支援
している。
[Conventional technology] Conventional fighter jets do not have a function to determine attack results to support air-to-air combat training, and in order to conduct air-to-air combat training, radar installed on the ground is required. Alternatively, measuring the relative position of an aircraft conducting combat training using a ground-based radio positioning device that determines the position of the aircraft by receiving radio waves transmitted from the aircraft conducting combat training, and determining the attack results, etc. supports air-to-air combat training.

[発明が解決しようとする課題] 上記のような従来の地上のレークもしくは無線位置標定
装置の支援による空対空戦闘訓練の可能な訓練空域は、
この地上のレークもしくは無線位置標定装置の上空に限
定されていた。
[Problem to be Solved by the Invention] The training airspace where air-to-air combat training can be conducted with the support of conventional ground rake or radio positioning equipment as described above is:
It was confined to the air above this ground rake or radio location device.

この発明は上記のような課題を解消するためになされた
もので、地上のレーダもしくは無線位置標定装置に依存
することなく5戦闘機の飛行可能な空域で戦闘訓練がで
きる戦闘機に搭載された空対空戦闘訓練支援装置を得る
ことを目的とする。
This invention was made to solve the above problems, and was installed on a fighter aircraft that can conduct combat training in an airspace where five fighter aircraft can fly without relying on ground radar or radio positioning equipment. The purpose is to obtain air-to-air combat training support equipment.

[課題を解決するための手段] この発明に係わる空対空戦闘訓練支援装置は。[Means to solve the problem] The air-to-air combat training support device according to this invention is:

目標機となった空対空戦闘訓練の相手戦闘機に対する方
位信号を照準方位信号を出力する火器管制装置と、火器
発射スイッチ部と、目標機の撃墜判定信号を入力して目
標機に対し特定の電波諸元の妨害波を出力するレーダ妨
害装置と、空対空戦闘訓練を実施している相手戦闘機の
レーダが自機を追尾しかつレーダ妨害装置が自機に妨害
波を出力していることを検出し、その妨害波の電波諸元
を出力するレーダ警戒装置と、撃墜もしくは被撃墜の戦
闘結果をパイロットへ伝達する戦果表示部と、記録部と
、火器発射スイッチ部からの火器発射信号の入力時に火
器管制装置から入力される目標機に対する方位信号と照
準方位信号との一致状態により攻撃の成否を判定し判定
結果を記録部へ出力し1判定結果が成功のときは撃墜判
定信号を戦果表示部とレーダ妨害装置に対して出力する
攻撃状態判定機能とレーダ警戒装置から出力される攻撃
戦闘機の妨害波の電波諸元をモニタし、この電波諸元が
あらかじめ指定されていた電波諸元と同一の場合自機が
撃墜されたものと判定し被撃墜信号を戦果表示部と記録
部へ出力する目標状態判定機能を有する訓練支援処理装
置とを具備したものである。
A fire control device that outputs a direction signal, a firearm firing switch unit, and a fire control device that outputs a direction signal to an opponent fighter aircraft in air-to-air combat training that was a target aircraft, and a fire control device that inputs a shoot-down judgment signal of the target aircraft and sends a specific target to the target aircraft. A radar jamming device that outputs jamming waves based on radio wave specifications, and the radar of an opponent fighter jet conducting air-to-air combat training are tracking the own aircraft, and the radar jamming device is outputting jamming waves to the own aircraft. a radar warning device that detects and outputs the radio wave specifications of the interference waves, a battle result display section that transmits the battle result of shooting down or being shot down to the pilot, a recording section, and a firearm firing signal from the firearm firing switch section. At the time of input, the success or failure of the attack is determined based on the matching state of the direction signal for the target aircraft inputted from the fire control system and the aiming direction signal, and the judgment result is output to the recording section.If the first judgment result is successful, the shoot-down judgment signal is sent as a battle result. Monitors the radio wave specifications of the attack fighter's interference waves output from the display unit and radar jamming device and the attack state judgment function output from the radar warning device, and this radio wave specification is the radio wave specification that was specified in advance. The training support processing device is equipped with a target state determination function that determines that the own aircraft has been shot down and outputs a shot-down signal to the battle results display section and the recording section.

「作用] この発明においては、火器管制装置は目標機に対する方
位信号及び照準方位信号を、火器発射スイッチ部は火器
発射信号をそれぞれ訓練支援処理装置に出力する。訓練
支援処理装置は、この火器発射信号の入力時における目
標機に対する方位信号と照準方位信号の一致状態により
撃墜の成否の判定を行い1判定結果を記録部に出力し2
判定結果が撃墜成功の場合には撃墜判定信号を戦果表示
部とレーダ妨害装置に対して出力する。レーク妨害装置
は、撃墜判定信号を入力した場合のみ特定の電波諸元の
妨害波の送信を一定期間目標機に対して行う。レーダ警
戒装置は、レーダ波及び妨害波を常時受信し、自機に対
するレーダ波の追尾および妨害波の出力を検出するとと
もに、その妨害波の電波諸元を訓練支援処理装置に対し
出力する。訓練支援処理装置はレーダ警戒装置から人力
された妨害波の電波諸元と、あらかじめ設定されていた
電波諸元とを比較し、これらの電波諸元が同一の場合撃
墜されたものと判定し、被撃墜信号を戦果表示部と記録
部へ出力する。
"Function" In the present invention, the fire control device outputs an azimuth signal and aiming direction signal for the target aircraft, and the firearm firing switch unit outputs a firearm firing signal to the training support processing device. The success or failure of shooting down is determined based on the matching state of the azimuth signal for the target aircraft and the aiming azimuth signal at the time of signal input, and 1 outputs the determination result to the recording section.
If the determination result is a successful shot down, a shot down determination signal is output to the battle result display section and the radar jamming device. The rake jamming device transmits jamming waves with specific radio wave specifications to the target aircraft for a certain period of time only when a shoot-down determination signal is input. The radar warning device constantly receives radar waves and jamming waves, detects tracking of the radar waves toward its own aircraft and output of the jamming waves, and outputs the radio wave specifications of the jamming waves to the training support processing device. The training support processing device compares the radio wave specifications of the interference waves manually input from the radar warning device with the radio wave specifications set in advance, and determines that the aircraft has been shot down if these radio wave specifications are the same. Outputs the shot down signal to the battle results display section and recording section.

[実施例] 第1図は、この発明の空対空戦闘訓練支援装置の一実施
例を示すブロック図である。
[Embodiment] FIG. 1 is a block diagram showing an embodiment of the air-to-air combat training support device of the present invention.

第1図において(1)は、目標機の方位と距離を測定す
るレーダ (2)、自機の機首方向と加速度を測定する
姿勢する姿勢加速度測定部(3)、目標機の位置とこの
目標機に対する照準方位を表示するヘッドアップディス
プレイ(5)、レーダ (2)から人力される目標機の
方位信号と距離信号と姿勢加速度測定部(3)から入力
される自機の角加速度信号と加速度信号とを処理して目
標機の位置信号と照準方位信号をヘッドアップディスプ
レイ(5)へ出力する火器管制信号処理部(4)から構
成される火器管制装置、(7)は火器の発射信号を出力
する火器発射スイッチ部、(8)は攻撃の成果と被撃墜
の記録を行う記録部、(9)は入力信号によって撃墜も
しくは被撃墜の音声信号を発生する音声信号発生部(1
0) 、音声信号の増幅を行う音声増幅部(11)及び
音声信号を音波として送出するヘッドセット(12)か
らなる戦果表示部、  (131は妨害波を送信する妨
害波送信アンテナ (14) 、妨害波送信機 (15
)及び撃墜判定信号の入力により特定の電波諸元の妨害
波を妨害波送信機(15)に出力させる妨害波制御部(
16)からなるレーダ妨害装置。
In Figure 1, (1) is a radar that measures the heading and distance of the target aircraft (2), an attitude acceleration measurement unit (3) that measures the nose direction and acceleration of the own aircraft, and a radar that measures the heading and acceleration of the target aircraft. A head-up display (5) that displays the aiming direction for the target aircraft, a direction signal and distance signal of the target aircraft manually input from the radar (2), and an angular acceleration signal of the own aircraft input from the attitude acceleration measurement unit (3). A fire control system consisting of a fire control signal processing unit (4) that processes the acceleration signal and outputs the target aircraft's position signal and aiming direction signal to the head-up display (5); (7) is a firearm firing signal; (8) is a recording section that records the results of the attack and shot down; (9) is an audio signal generation section (1) that generates an audio signal of shooting down or being shot down depending on the input signal;
0), a battle result display section consisting of an audio amplification section (11) that amplifies the audio signal and a headset (12) that sends out the audio signal as a sound wave; (131 is a jamming wave transmitting antenna (14) that transmits jamming waves; Interference wave transmitter (15
) and a jamming wave control unit (
16) A radar jamming device consisting of:

(17)は空対空戦闘訓練を行っている戦闘機のレーダ
波及び妨害波を受信する受信アンテナ(18) 、受信
機 F19) 、受信したレーダ波及び妨害波から攻撃
戦闘機のレーダによる追尾及び攻撃戦闘機からの妨害波
の出力を検波し、この妨害波の電波諸元を出力する受信
波処理部(20)とからなるレーク警戒装置。(6)は
火器発射スイッチ部(7)からの火器発射信号の人力さ
れたときにおける火器管制装置(1)の火器管制信号処
理部(4)から人力される目標機に対する方位信号と照
準方位信号との一致状態により攻撃の成否を判定し、こ
の判定結果を記録部(8)へ人力させ、この攻撃の判定
結果が成功の時は撃墜判定信号を戦果表示部(9)の音
声信号発生部(10)とレーダ妨害装置(13)の妨害
波制御部け6)へ出力する攻撃状態判定機能とレーダ警
戒装置(17)の出力する妨害波の電波諸元をモニタし
、この妨害波の電波諸元とあらかじめ設定されていた電
波諸元を比較し、これらが同一の場合自機が撃墜された
ものと判定し被撃墜信号を戦果表示部(9)の音声信号
発生部(10)と記録部(8)へ出力する目標状態判定
機能とを備えた訓練支援処理装置である。
(17) is a receiving antenna (18), receiver F19) that receives radar waves and jamming waves from fighter jets conducting air-to-air combat training, and a radar tracking and jamming wave of attacking fighter jets from the received radar waves and jamming waves. A rake warning device comprising a received wave processing unit (20) that detects the output of interference waves from an attack fighter and outputs the radio wave specifications of the interference waves. (6) refers to the direction signal and aiming direction signal for the target aircraft which are manually input from the fire control signal processing unit (4) of the fire control system (1) when the firearm discharge signal from the firearm discharge switch unit (7) is input manually. The success or failure of the attack is determined based on the matching state, and this determination result is manually transmitted to the recording section (8), and when the determination result of this attack is successful, a shoot-down determination signal is sent to the audio signal generation section of the battle result display section (9). (10) and the attack state determination function output to the jamming wave control section of the radar jamming device (13) (6), and monitor the radio wave specifications of the jamming wave output from the radar warning device (17), and monitor the radio waves of this jamming wave. The specifications are compared with the radio wave specifications set in advance, and if they are the same, it is determined that the own aircraft has been shot down, and the shot down signal is recorded in the audio signal generation section (10) of the battle results display section (9). This is a training support processing device equipped with a target state determination function that outputs output to the section (8).

第2図は、空対空戦闘訓練におりるこの発明の運用状態
の説明図である。第2図において (21)は攻撃状態
にある戦闘機(以下「攻撃機」という。) 、  (2
2)は目標機、  +231は攻撃機(21)の機首方
向であり弾丸もしくはミサイルの発射方向、  +24
)は攻撃機、  F21)の火器管制装置のレーダ (
2)により測定された目標機(22)の方位。
FIG. 2 is an explanatory diagram of the operational state of the present invention during air-to-air combat training. In Figure 2, (21) is a fighter aircraft in attack state (hereinafter referred to as "attack aircraft"), (2
2) is the target aircraft, +231 is the nose direction of the attack aircraft (21) and is the firing direction of the bullet or missile, +24
) is the radar of the fire control system of the F21) attack aircraft (
2) The bearing of the target aircraft (22) measured by.

(25)は攻撃機(21)においてレーダから入力され
る目標機の方位及び距離と姿勢加速度測定部(3)から
入力される自機の加速度及び角加速度を火器管制信号処
理部(4)が処理してヘッドアップディスプレイ(5)
に入力し表示させた照準方位信号である。
(25) In the attack aircraft (21), the fire control signal processing unit (4) receives the direction and distance of the target aircraft input from the radar and the acceleration and angular acceleration of the own aircraft input from the attitude acceleration measurement unit (3). Process and head up display (5)
This is the aiming direction signal input and displayed.

目標機(22)の方位(24)と照準方位(25)が致
しでいるときに、攻撃機(21)が火器を発射すると攻
撃機(21)の機首方向(23)と目標機(22)の飛
行方向との交点において火器が目標機(22)に命中す
る。
When the target aircraft (22)'s heading (24) and the aiming direction (25) are aligned, if the attack aircraft (21) fires a firearm, the nose direction (23) of the attack aircraft (21) and the target aircraft (22) ) the firearm hits the target aircraft (22) at the intersection with the flight direction.

空対空戦闘訓練を実施している攻撃機(21)にオイて
は、火器発射スイッチ部(7)のパイロット操作時に目
標機(22)の方位(24)と照準方位(25)の信号
が一致している場合に、訓練支援処理装置(6)は目標
機(22)を撃墜したものと判定し撃墜判定信号を発生
し、攻撃機(21)のレーダ妨害装置 (13)はこの
撃墜判定信号による妨害波測定部(16)の制御信号に
より特定の電波諸元の妨害波を出力する。
In an attack aircraft (21) conducting air-to-air combat training, when the pilot operates the firearm firing switch section (7), the direction (24) and aiming direction (25) signals of the target aircraft (22) are synchronized. If the target aircraft (22) has been shot down, the training support processing device (6) determines that the target aircraft (22) has been shot down and generates a shoot-down judgment signal, and the radar jamming device (13) of the attack aircraft (21) receives this shoot-down judgment signal. The control signal of the interference wave measurement unit (16) outputs interference waves with specific radio wave specifications.

攻撃機(21)に相対する目標機 (22)において、
レーダ警戒装置(17)は攻撃機(21)のレーダの追
尾状態及び攻撃機(21)からの妨害波の出力を検出し
、この妨害波の電波諸元を訓練支援処理装置(6)へ出
力する。次いで訓練支援処理装置(6)では、この妨害
波の電波諸元とあらかじめ設定されていた電波諸元とを
比較し、これらが同一の時自機が撃墜されたものと判定
し、被撃墜信号を戦果表示部(9)及び記録部(8)に
出力する。
In the target aircraft (22) facing the attack aircraft (21),
The radar warning device (17) detects the radar tracking state of the attack aircraft (21) and the output of interference waves from the attack aircraft (21), and outputs the radio wave specifications of this interference wave to the training support processing device (6). do. Next, the training support processing device (6) compares the radio wave specifications of this interference wave with preset radio wave specifications, and when these are the same, it determines that the own aircraft has been shot down, and transmits the shot down signal. is output to the result display section (9) and the recording section (8).

[発明の効果] 以上のようにこの発明によれば、空対空戦闘訓練におい
て地上の位置標定装置等に依存することなく1戦闘機の
飛行できる全区域での支援を1戦闘機搭載された空対空
戦闘訓練支援装置により行うことができる。
[Effects of the Invention] As described above, according to the present invention, in air-to-air combat training, support can be provided in all areas over which one fighter can fly, without relying on ground positioning devices, etc. This can be done using anti-aircraft combat training support equipment.

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

第1図はこの発明の一実施例を示す空対空戦闘訓練支援
装置のブロック図、第2図はこの発明による装置の運用
状態の説明図である。 図中(1)は火器管制装置、(2)はレーダ、(3)は
姿勢加速度測定部、(4)は火器管制信号処理部。 (5)はヘッドアップディスプレイ、(6)は訓練支援
処理装置、(7)は火器発射スイッチ部、(8)は記録
部、(9)は戦果表示部、  flolは音声信号発生
部、 (ii)は音声増幅部、  (12)はへラドセ
ット。 (13)はレーダ妨害装置、  (14)は妨害送信ア
ンテナ、 f15)は妨害波送信機、 (161は妨害
波制御部。 (17)はレーダ警戒装置、  f181は受信アンテ
ナ。 (19)は受信機、  (20)は受信波処理部、  
(21)は攻撃機、 (22+は目標機、 (23)は
機首方向、  (24)は目標の方位、  (25)は
照準方位である。
FIG. 1 is a block diagram of an air-to-air combat training support device showing an embodiment of the present invention, and FIG. 2 is an explanatory diagram of the operating state of the device according to the present invention. In the figure, (1) is a fire control device, (2) is a radar, (3) is an attitude acceleration measurement unit, and (4) is a fire control signal processing unit. (5) is a head-up display, (6) is a training support processing device, (7) is a firearm firing switch section, (8) is a recording section, (9) is a battle result display section, flol is an audio signal generation section, (ii ) is the audio amplification unit, and (12) is the Herad set. (13) is a radar jamming device, (14) is a jamming transmitting antenna, f15) is a jamming wave transmitter, (161 is a jamming wave control unit. (17) is a radar warning device, and f181 is a receiving antenna. (19) is a receiving antenna. (20) is a received wave processing section,
(21) is the attack aircraft, (22+ is the target aircraft, (23) is the nose direction, (24) is the target direction, and (25) is the aiming direction.

Claims (1)

【特許請求の範囲】[Claims] 空対空戦闘訓練において自機の攻撃目標となった目標戦
闘機を追尾し、この目標戦闘機に対する方位信号と距離
信号を出力するレーダ、上記レーダからの方位信号と距
離信号を入力処理して上記目標戦闘機の方位信号と照準
方位信号を発生する火器管制信号処理部、上記目標戦闘
機に対する方位と照準方位を表示するヘッドアップディ
スプレイとを有する火器管制装置と、上記目標戦闘機の
撃墜判定信号を入力して上記目標戦闘機に対し特定の電
波諸元の妨害波を出力するレーダ妨害装置と、自機を攻
撃目標とした攻撃戦闘機のレーダ波及び妨害波を受信し
て、攻撃戦闘機のレーダが自機を追尾しかつ上記レーダ
妨害装置が自機に妨害波を出力していることを検出する
とともに、その妨害波の電波諸元を出力するレーダ警戒
装置と、パイロットのスイッチ操作により火器発射信号
を出力する火器発射スイッチ部と、撃墜及び被撃墜の戦
闘結果をパイロットへ伝達する戦果表示部と、戦闘結果
を記録する記録部と、上記火器発射スイッチ部からの信
号入力時における上記火器管制装置からの目標戦闘機に
対する方位信号と照準方位信号との一致状態により攻撃
の成否を判定し、その判定結果を上記記録部へ出力し、
判定結果が攻撃成功の場合は上記目標戦闘機の撃墜判定
信号を上記戦果表示部へ出力するとともに、上記撃墜判
定信号を上記レーダ妨害装置へ出力する攻撃状態判定機
能と上記レーダ警戒装置から出力される攻撃戦闘機の妨
害波の電波諸元をモニタし、この電波諸元があらかじめ
設定されていた電波諸元と同一の場合自機が撃墜された
ものと判定し、被撃墜信号を上記戦果表示部と記録部へ
出力する目標状態判定機能を有する訓練支援処理装置と
を戦闘機に搭載したことを特徴とする空対空戦闘訓練支
援装置。
A radar that tracks a target fighter that is the attack target of its own aircraft during air-to-air combat training, and outputs a direction signal and a distance signal to this target fighter, and inputs and processes the direction signal and distance signal from the radar. a fire control device having a fire control signal processing unit that generates a bearing signal and an aiming direction signal for the target fighter, a head-up display that displays the bearing and aiming direction for the target fighter; and a shoot-down determination signal for the target fighter. A radar jamming device that outputs jamming waves with specific radio wave specifications to the target fighter by inputting A radar warning device that detects that the radar is tracking the own aircraft and that the radar jamming device is outputting interference waves to the own aircraft, and outputs the radio wave specifications of the interference waves, and a radar warning device that detects that the radar is tracking the own aircraft and outputs the radio wave specifications of the interference waves, and the pilot operates a switch. a firearm firing switch unit that outputs a firearm firing signal; a battle result display unit that transmits the battle results of shot down and shot down to the pilot; a recording unit that records the battle results; Determining the success or failure of the attack based on the matching state of the azimuth signal for the target fighter aircraft from the fire control device and the aiming azimuth signal, and outputting the determination result to the recording section,
If the determination result is a successful attack, an attack status determination function outputs a shot-down determination signal of the target fighter to the battle result display section, and an attack state determination function that outputs the shot-down determination signal to the radar jamming device, and output from the radar warning device. monitors the radio wave specifications of the jamming waves of the attack fighter, and if these radio wave specifications are the same as the radio wave specifications set in advance, it is determined that the own aircraft has been shot down, and the shot down signal is displayed on the above-mentioned battle results display. What is claimed is: 1. An air-to-air combat training support system, characterized in that a fighter aircraft is equipped with a training support processing system having a function of determining a target state and outputting to a recording part.
JP9806290A 1990-04-13 1990-04-13 Air-to-air fight training supporting apparatus Pending JPH04194A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9806290A JPH04194A (en) 1990-04-13 1990-04-13 Air-to-air fight training supporting apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9806290A JPH04194A (en) 1990-04-13 1990-04-13 Air-to-air fight training supporting apparatus

Publications (1)

Publication Number Publication Date
JPH04194A true JPH04194A (en) 1992-01-06

Family

ID=14209842

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9806290A Pending JPH04194A (en) 1990-04-13 1990-04-13 Air-to-air fight training supporting apparatus

Country Status (1)

Country Link
JP (1) JPH04194A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103851960A (en) * 2013-12-28 2014-06-11 中国人民解放军沈阳炮兵学院 Small linear antenna capable of simulating generation of trajectory target signal

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103851960A (en) * 2013-12-28 2014-06-11 中国人民解放军沈阳炮兵学院 Small linear antenna capable of simulating generation of trajectory target signal

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