JPS62268999A - Air-to-air combat training supporter - Google Patents

Air-to-air combat training supporter

Info

Publication number
JPS62268999A
JPS62268999A JP11154086A JP11154086A JPS62268999A JP S62268999 A JPS62268999 A JP S62268999A JP 11154086 A JP11154086 A JP 11154086A JP 11154086 A JP11154086 A JP 11154086A JP S62268999 A JPS62268999 A JP S62268999A
Authority
JP
Japan
Prior art keywords
signal
fighter
radar
target
aircraft
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
Application number
JP11154086A
Other languages
Japanese (ja)
Other versions
JPH0419480B2 (en
Inventor
康弘 大嶋
香田 ▲あきら▼
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.)
Japan Steel Works Ltd
Mitsubishi Electric Corp
Technical Research and Development Institute of Japan Defence Agency
Original Assignee
Japan Steel Works Ltd
Mitsubishi Electric Corp
Technical Research and Development Institute of Japan Defence Agency
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 Japan Steel Works Ltd, Mitsubishi Electric Corp, Technical Research and Development Institute of Japan Defence Agency filed Critical Japan Steel Works Ltd
Priority to JP11154086A priority Critical patent/JPS62268999A/en
Publication of JPS62268999A publication Critical patent/JPS62268999A/en
Publication of JPH0419480B2 publication Critical patent/JPH0419480B2/ja
Granted 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〕 この発明は9戦闘機パイロットが戦闘機を用いた空対空
戦闘訓練を行う時に使用し、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] [Field of Industrial Application] This invention is an air-to-air combat training support that is used by nine fighter pilots to conduct air-to-air combat training using fighter aircraft, and supports air-to-air combat training. It is related to the device.

〔従来の技術〕[Conventional technology]

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または
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全測定し、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 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, radars installed on the ground or combat training are used. Air-to-air combat is achieved by measuring the relative positions of aircraft conducting combat training using ground-based radio positioning equipment that receives radio waves transmitted from aircraft and determines the aircraft's position. Supporting training.

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

上記のような従来の地上のレーダまたは無線位置標定装
置の支援による空対空戦闘訓練の可能な訓練空域は、こ
の地上レーダまたは無線位置標定装置の周辺の上空に限
定されるという問題点があった。
There is a problem in that the training airspace in which air-to-air combat training can be carried out with the support of conventional ground radar or radio positioning equipment as described above is limited to the upper skies around the ground radar or radio positioning equipment. .

この発明は、かかる問題点を解決するためになされたも
のであυ、地上のレーダまたは無線位置標定装置に依存
することなく1戦闘機の飛行可能な空域で空対空戦闘訓
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
を得ること金目的とする。
This invention was made to solve these problems, and is designed to provide a fighter aircraft that can conduct air-to-air combat training in an airspace where a single fighter aircraft can fly without relying on ground radar or radio positioning equipment. The objective is to obtain an onboard air-to-air combat training support system.

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

この発明に係わる空対空戦闘訓練支援装置は空対空戦闘
訓練において自機の攻撃目標となった目標機闘機を追尾
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、前記レーダからの方位信号と距離信号を用
いて上記目標戦闘機の位置信号と照準方位信号を発生し
、また目標戦闘機の撃墜判定信号を入力して追尾状態の
上記レーダの電波諸元を変化させる制御信号を発生する
火器管制信号処理部および上記目標戦闘機に対する万位
と照準方位を表示する表示部とを有する火器管制装置と
、自機を攻撃目標とした攻撃戦闘機のレーダ波を受信し
て攻撃戦闘機のレーダが自機を追尾していることを検出
するとともにそのレーダの電波諸元を出力するレーダ警
戒装置と、パイフ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、撃墜と被撃墜の戦
闘結果をパイロットへ伝達する戦果表示部と9戦闘結果
を記鎌する記録部と、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
の成否を判定し判定結果を上記記録部へ入力し1判定結
果が攻撃成功のときは上記目標戦闘機の撃墜判定信号全
上記戦果表示部へ入力させるとともに上記撃墜判定信号
を上記火器管制装置へ入力させ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レーダの
電波諸元をモニタし、この電波諸元の変化を検出するこ
とによp自機が撃墜されたものと判定し被撃墜判定信号
を上記戦果表示部と上記記録部とへ入力させる目標状態
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。
The air-to-air combat training support device according to the present invention includes a radar that tracks a target fighter aircraft that is an attack target of its own aircraft during air-to-air combat training, and outputs a direction signal and a distance signal to the target fighter aircraft; A control signal that generates a position signal and an aiming direction signal of the target fighter using the azimuth signal and distance signal of the target fighter, and inputs a shot-down determination signal of the target fighter to change the radio wave specifications of the radar in a tracking state. A fire control device having a fire control signal processing unit that generates a fire control signal processing unit and a display unit that displays the direction and aiming direction for the target fighter aircraft, and a fire control device that receives radar waves of an attack fighter targeting the own aircraft and attacks. A radar warning device that detects that a fighter jet's radar is tracking the aircraft and outputs the radar's radio wave specifications, a firearm firing switch unit that outputs a firearm firing signal by operating a pie foot switch, and a battle results display section that transmits the battle results of being shot down to the pilot; a recording section that records the battle results; and a direction signal and aiming toward the target fighter plane from the fire control device when a signal is input from the firearm firing switch section. The success or failure of the attack is determined based on the state of coincidence with the azimuth signal, and the determination result is input to the recording section, and if the first determination result is a successful attack, the shot down determination signal of the target fighter is all input to the battle result display section, and the shot down is The attack state determination function inputs a determination signal to the fire control device, and the radio wave specifications of the attack fighter's radar output from the radar warning device are monitored, and changes in the radio wave specifications are detected. The apparatus is equipped with a training support processing device having a target state determination function that determines that the aircraft has been shot down and inputs a shot down determination signal to the result display section and the recording section.

〔作用〕[Effect]

この発明においては、火器管制装置は目標機の方位信号
とfI@準方位信号とを、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へ入力させる。訓練
支援処理装置は、この火器発射信号が入力された時のこ
の目標戦闘機の方位信号と照準方位信号との一致状態に
より攻撃の成否の判定を行い9判定結果を記録部へ入力
させ1判定結果が攻撃成功のときは9$墜判定信号を戦
果表示部と火器管制装置とへ入力させる。火器管制装置
は、撃墜判定信号の入力により追尾状態のレーダの電波
諸元を変化させ目標戦闘機へ撃墜判定信号を伝送する。
In this invention, the fire control device inputs the target aircraft's azimuth signal and the fI@sub-azimuth signal, and the firearm firing switch section inputs the firearm firing signal to the training support processing device. The training support processing device determines the success or failure of the attack based on the matching state of the target fighter's azimuth signal and the aiming azimuth signal when this firearm firing signal is input, inputs the result of 9 determinations to the recording section, and makes 1 determination. If the result is a successful attack, a 9$ crash determination signal is input to the battle result display section and the fire control device. The fire control device changes the radio wave specifications of the radar in the tracking state upon input of the shoot-down judgment signal, and transmits the shoot-down judgment signal to the target fighter aircraft.

またレーダ警戒装置は、攻撃戦闘機の火器管制装置のレ
ーダが自機を追尾していることを検出し。
In addition, the radar warning system detects that the radar of the attack fighter's fire control system is tracking the aircraft.

とのレーダの電波諸元を訓練支援処理装置へ入力させる
。訓練支援処理装置は、この入力されたレーダの電波諸
元をモニタし、レーダの電波諸元の変化を検出すること
により自機が撃墜されたものと判定し、被撃墜判定信号
を戦果表示部と記録部へ入力させる。
input the radio wave specifications of the radar into the training support processing device. The training support processing device monitors the input radar radio wave specifications, determines that its own aircraft has been shot down by detecting changes in the radar radio wave specifications, and sends the shot down determination signal to the battle results display section. input into the recording section.

〔実施例〕〔Example〕

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。
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)は目標戦闘機の方位と距離を測
定し後述する制御信号により追尾状態の電波諸元を変化
するレーダ(2)と自機の機首方向と加速度を測定する
姿勢加速度測定部(3)とこのレーダ(21から入力さ
れる方位信号、距離信号と上記姿勢加速度測定部(3)
から入力される角加速度信号、加速度信号とにより目標
戦闘機の位置信号と照準方位信号とを発生し入力される
撃墜判定信号により上記レーダへ制御信号を出力する火
器管制信号処理部(4)とこの火器管制信号処理部(4
)から入力される目標戦闘機の位置信号と照準方位信号
の表示を行うヘッドアップディスプレイ(5)とからな
る火器管制装置、(6)はレーダ波受信アンテナ(7)
とレーダ波受信機(8)と自機を追尾しているレーダ波
を検出しそのレーダ波の電波諸元を出力するレーダ波処
理部(9)とからなるレーダ警戒装置と、 QQはパイ
ロットの操作により火器の発射信号を出力する火器発射
スイッチ部、aυは入力信号によって撃墜または被撃墜
の音声信号を発生する音声信号発生部α3とこの音声信
号を増幅する音声増幅部(3)とこの増幅された音声信
号を音波として送出するヘッドセット04とからなる戦
果表示部、(1っけ攻撃の判定結果と自機の被撃墜とを
記録する記録部、 (Leは上記火器発射スイッチ部α
1からの火器発射信号入力時における上記火器管制装置
(1)からの入力信号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判
定結果を上記記録部(I9へ入力させ攻撃成功のときは
撃墜判定信号を上記戦果表示部aυへと上記レーダ(2
)の電波諸元を変化させるため上記火器管制信号処理部
(4)へと入力させる攻撃状態判定機能と上記レーダ警
戒装置(6)の入力するレーダの電波諸元をモニタしこ
のレーダの電波諸元の変化を検出し自機が撃墜されたも
のと判定し被撃墜判定信号を上記戦果表示部σカと上記
記録部09へ入力させ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。
In Figure 1, (1) is a radar that measures the direction and distance of the target fighter and changes the radio wave specifications in the tracking state based on control signals described later, and (2) the attitude that measures the nose direction and acceleration of the own aircraft. The acceleration measurement unit (3), the direction signal and distance signal input from this radar (21), and the attitude acceleration measurement unit (3)
a fire control signal processing unit (4) that generates a position signal and a aiming direction signal of the target fighter based on the angular acceleration signal and the acceleration signal inputted from the angular acceleration signal inputted from the target fighter, and outputs a control signal to the radar based on the inputted shoot-down determination signal; This fire control signal processing unit (4
) is a fire control system consisting of a head-up display (5) that displays the target fighter's position signal and aiming direction signal, which is input from a radar wave receiving antenna (7).
A radar warning system consisting of a radar wave receiver (8), a radar wave processing unit (9) that detects radar waves tracking the own aircraft and outputs the radio wave specifications of the radar waves, and QQ is the pilot's Firearm firing switch unit that outputs a firearm firing signal when operated, aυ is an audio signal generating unit α3 that generates an audio signal indicating shooting down or being shot down depending on the input signal, an audio amplification unit (3) that amplifies this audio signal, and this amplification. A battle result display section consisting of a headset 04 that sends out the voice signal as a sound wave, a recording section that records the judgment result of a one-shot attack and whether your own aircraft was shot down, (Le is the firearm firing switch section α
The success or failure of the attack is determined based on the matching state of the azimuth signal for the target fighter and the aiming azimuth signal of the input signal from the fire control device (1) when the firearm firing signal is input from the I9. When the attack is successful, the shot down judgment signal is sent to the above-mentioned battle result display section aυ and the above-mentioned radar (2
) to change the radio wave specifications of the radar, the attack state determination function inputs the signal to the fire control signal processing section (4), and the radar radio wave specifications input to the radar warning device (6) are monitored and the radio wave specifications of this radar are changed. This training support processing device is equipped with a target state determination function that detects a change in the original value, determines that the own aircraft has been shot down, and inputs a shot down determination signal to the above-mentioned battle result display section σ and the above-mentioned recording section 09.

第2図は空対空戦闘訓練の状態を示す図であシ。Figure 2 is a diagram showing the state of air-to-air combat training.

図においてC311は攻撃戦闘機、 03は目標戦闘機
、03は攻撃戦闘機Gυの機首方向であシ弾丸またはミ
サイルの発射方向、(ロ)は攻撃戦闘機clDの火器管
制装置のレーダ(2)により測定された目標戦闘機C3
3の方位、(至)は攻撃戦闘機Gυにおいてレーダ(2
)から入力される目標戦闘機G3の方位と距離との信号
と姿勢加速度HH1;定部(3)から入力される自機の
加速度と角速度との信号とを火器管制信号処理部(4)
が処理をしてヘッドアップディスプレイ(5)に入力さ
せ表示させた照準方位、(至)は攻撃戦闘機Gυにおけ
る目標戦闘機G3の方位測定と攻撃戦闘機C311から
目標戦闘機G3への撃墜判定信号の伝送との機能を有す
る追尾状態のレーダの電波ビームである。
In the figure, C311 is an attack fighter, 03 is a target fighter, 03 is the nose direction of the attack fighter Gυ, the firing direction of bullets or missiles, and (b) is the radar (2) of the fire control system of the attack fighter CLD. ) target fighter C3 measured by
The direction of 3 (to) is the radar (2) of the attack fighter Gυ.
) and the attitude acceleration HH1 and the direction and distance signals of the target fighter aircraft G3 input from the fire control signal processing unit (4);
The aiming direction that was processed and input and displayed on the head-up display (5), (to) is the measurement of the direction of the target fighter G3 by the attack fighter Gυ and the shot down judgment from the attack fighter C311 to the target fighter G3. This is a radar radio wave beam in a tracking state that has the function of signal transmission.

上記目標戦闘機03の方位(ロ)と照準方位(イ)との
方位が一致しているときに攻撃戦闘機Co11が火器を
発射すると攻撃戦闘機G9の機首方向(ハ)と目標戦闘
機G3の飛行方向の交った点にて火器が目標戦闘機■に
命中する。
When attack fighter Co11 fires a firearm when the bearing of target fighter 03 (b) and the aiming bearing (a) match, the nose direction of attack fighter G9 (c) and the target fighter The firearm hits the target fighter ■ at the point where G3's flight directions intersect.

空対空戦闘訓練においては、攻撃戦8機Gelの火器発
射スイッチ部α1のスイッチが押された時の目標戦闘p
Acoの方位(至)と照準方位(至)との方位が一致し
ている場合に攻撃戦闘機Gυの訓練支援処理装置t1e
は目標戦闘機C3を撃墜したものと判定し撃墜判定の信
号を発生し、攻撃戦闘機Gl)のレーダはこの撃墜判定
の信号による火器管制信号処理部(4)の制御信号によ
りレーダ(2)の電波諸元を変化させる。
In air-to-air combat training, the target battle p when the gun firing switch part α1 of the 8 Gel attack aircraft is pressed.
When the direction of Aco (to) and the aiming direction (to) match, the training support processing device t1e of the attack fighter Gυ
determines that the target fighter C3 has been shot down and generates a signal indicating that the target fighter C3 has been shot down, and the radar of the attacking fighter Gl) uses the control signal of the fire control signal processing unit (4) based on this signal indicating that the target fighter aircraft G1 has been shot down. change the radio wave specifications.

上記攻撃戦闘機G′Dに相対する目標戦闘機G3におい
ては、レーダ警戒装置(6)は攻撃戦闘機C31)の追
尾状態のレーダのレーダ波を検出しこのレーダ波の電波
誌元を訓練支援処理装置utiへ入力させ、訓練支援処
理装置珀はこの入力された電波諸元の変化を検出し自機
が撃墜されたものと判定し被撃墜判定の信号を戦果表示
部(Il)と記録部αりに入力させる。
In the target fighter G3 facing the attack fighter G'D, the radar warning device (6) detects the radar wave of the radar tracking the attack fighter C31) and uses the radio wave source of this radar wave to provide training support. This is input to the processing unit uti, and the training support processing unit 珀 detects changes in the input radio wave specifications, determines that the own aircraft has been shot down, and sends a shot down determination signal to the battle result display unit (Il) and the recording unit. Let the user input the information.

〔発明の効果〕〔Effect of the invention〕

この発明は以上説明したとおシ、火器管制装置とレーザ
警戒装置と火器発射スイッチ部と戦果表示部と記録部と
これ等のそれぞれと接続された511練支援処理装置と
の構成により成る戦闘機搭載の装置であシ、地上の位置
標定装置等に依存することなく9戦闘機の飛行ができる
全空域での空対空戦闘Δ11練を可能にするものである
As described above, this invention is mounted on a fighter aircraft and is comprised of a fire control device, a laser warning device, a firearm firing switch section, a battle results display section, a recording section, and a 511 training support processing device connected to each of these sections. This device enables air-to-air combat Δ11 training in the entire airspace, where nine fighter aircraft can fly without relying on ground positioning equipment.

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

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
装置のブロックメ、第2図はこの発明による装置の運用
状態を示す図である。 図において、(1)は火器管制装置、C2)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)はレーダ警
戒装置、(7)はレーダ波受信アンテナ、(8Jはレー
ダ波受信機、(9)はレーダ波処理部、 QQは火器発
射スイッチ部、αυは訓練支援処理装置、 (I2は音
声信号発生部、(11は音声増幅部、α4はへラドセラ
)、(isは記録部、鰻は訓練支援処理装置、011は
攻撃戦闘機。 ■は目標戦闘機である。
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 a diagram showing the operating state of the device according to the present invention. In the figure, (1) is a fire control system, and C2) is a radar. (3) is an attitude acceleration measuring section, and (4) is a fire control signal processing section. (5) is a head-up display, (6) is a radar warning device, (7) is a radar wave receiving antenna, (8J is a radar wave receiver, (9) is a radar wave processing unit, QQ is a firearm firing switch unit, αυ is a training support processing unit, (I2 is an audio signal generation unit, (11 is an audio amplification unit, α4 is a heradocera), (is is a recording unit, eel is a training support processing unit, 011 is an attack fighter. ■ is a target combat It is a machine.

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つた目標戦
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、前記レーダからの方位信号と距
離信号を用いて上記目標戦闘機の位置信号と照準方位信
号を発生し、また目標戦闘機の撃墜判定信号を入力して
追尾状態の上記レーダの電波諸元を変化させる制御信号
を発生する火器管制信号処理部および上記目標戦闘機に
対する方位と照準方位を表示する表示部とを有する火器
管制装置と、自機を攻撃目標とした攻撃戦闘機のレーダ
波を受信して攻撃戦闘機のレーダが自機を追尾している
ことを検出するとともにそのレーダ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、撃墜と
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判定結果を上記記録部へ入力
し、判定結果が攻撃成功のときは上記目標戦闘機の撃墜
判定信号を上記戦果表示部へ入力させるとともに上記撃
墜判定信号を上記火器管制装置へ入力させる攻撃状態判
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
のレーダの電波諸元をモニタし、この電波諸元の変化を
検出することにより自機が撃墜されたものと判定し被撃
墜判定信号を上記戦果表示部と上記記録部とへ入力させ
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 the target fighter, and uses the direction signal and distance signal from the radar to target the target fighter. A fire control signal processing unit that generates the aircraft's position signal and aiming direction signal, and also inputs the target fighter's shootdown determination signal and generates a control signal that changes the radio wave specifications of the radar in the tracking state; and the target combat aircraft. A fire control device that has a display unit that displays the direction and aiming direction for the aircraft, and the radar of the attack fighter that tracks the aircraft by receiving the radar waves of the attack fighter that targets the aircraft. A radar warning device that detects and outputs the radio wave specifications of the radar, a firearm firing switch unit that outputs a firearm firing signal by the pilot's switch operation, and a battle results display unit that transmits the battle results of shot down and shot down to the pilot. and a recording unit that records the battle results, and a determination unit that determines 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 when the signal is input from the firearm firing switch unit. an attack state determination function that inputs the result to the recording section, and when the determination result is a successful attack, inputs a shot down determination signal of the target fighter to the battle result display section and inputs the shot down determination signal to the fire control device; It monitors the radio wave specifications of the radar of the attack fighter output from the radar warning system, and by detecting changes in the radio wave specifications, it determines that its own aircraft has been shot down, and sends a shot down determination signal to the above-mentioned battle results. An air-to-air combat training support device, characterized in that a training support processing device having a display unit and a target state determination function for inputting information to the recording unit is mounted on a fighter aircraft.
JP11154086A 1986-05-15 1986-05-15 Air-to-air combat training supporter Granted JPS62268999A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11154086A JPS62268999A (en) 1986-05-15 1986-05-15 Air-to-air combat training supporter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11154086A JPS62268999A (en) 1986-05-15 1986-05-15 Air-to-air combat training supporter

Publications (2)

Publication Number Publication Date
JPS62268999A true JPS62268999A (en) 1987-11-21
JPH0419480B2 JPH0419480B2 (en) 1992-03-30

Family

ID=14563953

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11154086A Granted JPS62268999A (en) 1986-05-15 1986-05-15 Air-to-air combat training supporter

Country Status (1)

Country Link
JP (1) JPS62268999A (en)

Also Published As

Publication number Publication date
JPH0419480B2 (en) 1992-03-30

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