JPH0457095U - - Google Patents

Info

Publication number
JPH0457095U
JPH0457095U JP9842290U JP9842290U JPH0457095U JP H0457095 U JPH0457095 U JP H0457095U JP 9842290 U JP9842290 U JP 9842290U JP 9842290 U JP9842290 U JP 9842290U JP H0457095 U JPH0457095 U JP H0457095U
Authority
JP
Japan
Prior art keywords
target
flying object
tracking
seeker
mother 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.)
Pending
Application number
JP9842290U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP9842290U priority Critical patent/JPH0457095U/ja
Publication of JPH0457095U publication Critical patent/JPH0457095U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)

Description

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

第１図は本考案の一実施例の説明図、第２図は
上記一実施例の演算装置の詳細説明図、第３図は
従来のパイロツトの操作の説明図である。 １……母機レーダ、２……演算装置、３……母
機、４……減算器、５……積算器、６……加算器
、７……平方根演算器、８……判定器、９……シ
ーカ、１０……飛しよう体、１１……ターゲツト
、１２……フレアデコイ。 FIG. 1 is an explanatory diagram of one embodiment of the present invention, FIG. 2 is a detailed explanatory diagram of the arithmetic unit of the above-mentioned embodiment, and FIG. 3 is an explanatory diagram of the operation of a conventional pilot. DESCRIPTION OF SYMBOLS 1...Mother machine radar, 2...Arithmetic unit, 3...Mother machine, 4...Subtractor, 5...Integrator, 6...Adder, 7...Square root arithmetic unit, 8...Determiner, 9... ...Seeker, 10...Flying body, 11...Target, 12...Flare decoy.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 母機に設けられターゲツトの方向を検出する母
機レーダ、赤外線追尾飛しよう体に設けられター
ゲツトの方向を検出して同飛しよう体を誘導する
シーカ、上記母機に設えられ母機レーダ及びシー
カよりそれぞれが検出したターゲツト方向を入力
し上記飛しよう体をフレアデコイへの誤追尾から
ターゲツトへの追尾へ復帰させるスレーブ信号を
上記シーカへ出力する演算装置を備えたことを特
徴とする飛しよう体誤追尾自動復帰装置。 The mother aircraft radar installed on the mother aircraft detects the direction of the target, the seeker installed on the infrared tracking flying object detects the direction of the target and guides the flying object, and the mother aircraft radar and seeker installed on the above mother aircraft detect each other. A flying object tracking automatic return device characterized in that it is equipped with an arithmetic device which inputs the target direction and outputs a slave signal to the seeker to return the flying object from erroneous tracking to the flare decoy to tracking to the target. .
JP9842290U 1990-09-21 1990-09-21 Pending JPH0457095U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9842290U JPH0457095U (en) 1990-09-21 1990-09-21

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9842290U JPH0457095U (en) 1990-09-21 1990-09-21

Publications (1)

Publication Number Publication Date
JPH0457095U true JPH0457095U (en) 1992-05-15

Family

ID=31839600

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9842290U Pending JPH0457095U (en) 1990-09-21 1990-09-21

Country Status (1)

Country Link
JP (1) JPH0457095U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016173269A (en) * 2015-03-16 2016-09-29 三菱電機株式会社 Sensor control system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016173269A (en) * 2015-03-16 2016-09-29 三菱電機株式会社 Sensor control system

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