JPS6081497U - radar control system - Google Patents
radar control systemInfo
- Publication number
- JPS6081497U JPS6081497U JP17093983U JP17093983U JPS6081497U JP S6081497 U JPS6081497 U JP S6081497U JP 17093983 U JP17093983 U JP 17093983U JP 17093983 U JP17093983 U JP 17093983U JP S6081497 U JPS6081497 U JP S6081497U
- Authority
- JP
- Japan
- Prior art keywords
- aircraft
- specification information
- friendly
- control system
- transmitter
- 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
Links
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
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
第1図は、従来のレーダ管制システムの構成図、第2図
は第1図従来のレーダ管制システムの動作図、第3図は
この考案によるレーダ管制システムの構成図、第4図は
第3図この考案によるレーダ管制システムの動作図であ
る。図中1はアンテナ、2はトランスミッタ、3はレシ
ーバ、4はアナログ・プロセッサ、5はディジタル・シ
グナル・プロセッサ、6はレーダ・データ・プロセッサ
、7はセントラル・コンピュータ、8はヘッドアップ・
ディスプレイ、10はアンテナ、11はトランスミッタ
、12はレシーバである。なお、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。Fig. 1 is a block diagram of a conventional radar control system, Fig. 2 is an operational diagram of the conventional radar control system shown in Fig. 1, Fig. 3 is a block diagram of a radar control system according to this invention, and Fig. 4 is a block diagram of a radar control system according to the present invention. Figure 1 is an operational diagram of the radar control system according to this invention. In the figure, 1 is an antenna, 2 is a transmitter, 3 is a receiver, 4 is an analog processor, 5 is a digital signal processor, 6 is a radar data processor, 7 is a central computer, and 8 is a heads-up computer.
10 is an antenna, 11 is a transmitter, and 12 is a receiver. Note that the same or equivalent parts in the figures are indicated by the same reference numerals.
Claims (1)
置および上記電子装置で得られる情報をもとにして、目
標機との目標諸元情報および自機の諸元情報の算出を行
うセントラルコンピュータとを有する航空機のレーダ管
制システムにおいて上記セントラルコンピュータの各種
諸元情報をもとに所要の信号波を発生するトランスミッ
タと、上記トランスミッタの信号波を味方機方向に送信
しかつ味方機からの各種諸元情報を含む信号波を受ける
アンテナと、上記アンテナで受信した味方機からの各種
諸元情報を含む信号波を復調しかつその出力を上記セン
トラルコンピュータに与えるためのレシーバと、上記セ
ントラルコンピュータで処理された自機の諸元情報と味
方機の各種諸元情報を導入し、目標機に関する味方機の
追尾状況を表示するディスプレイ装置とを備えたことを
特徴とするレーダ管制システム。An electronic device for missile launch control and missile guidance, and a central computer that calculates target specification information for the target aircraft and specification information for the own aircraft based on the information obtained by the electronic device. A transmitter that generates the required signal waves based on various specification information of the central computer in the radar control system of the aircraft, and a transmitter that transmits the signal waves of the transmitter toward friendly aircraft and receives various specification information from the friendly aircraft. a receiver for demodulating the signal wave containing various specification information from friendly aircraft received by the antenna and giving its output to the central computer; A radar control system comprising a display device that introduces specification information of own aircraft and various specification information of friendly aircraft and displays tracking status of friendly aircraft with respect to a target aircraft.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17093983U JPS6081497U (en) | 1983-11-04 | 1983-11-04 | radar control system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17093983U JPS6081497U (en) | 1983-11-04 | 1983-11-04 | radar control system |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6081497U true JPS6081497U (en) | 1985-06-06 |
Family
ID=30373026
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP17093983U Pending JPS6081497U (en) | 1983-11-04 | 1983-11-04 | radar control system |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6081497U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0645929A (en) * | 1992-04-17 | 1994-02-18 | Hughes Aircraft Co | Divider of half of integer and low-noise frequency synthesizer using analog gain compensation |
JPH09203600A (en) * | 1996-01-26 | 1997-08-05 | Mitsubishi Electric Corp | Airframe guiding apparatus |
-
1983
- 1983-11-04 JP JP17093983U patent/JPS6081497U/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0645929A (en) * | 1992-04-17 | 1994-02-18 | Hughes Aircraft Co | Divider of half of integer and low-noise frequency synthesizer using analog gain compensation |
JPH09203600A (en) * | 1996-01-26 | 1997-08-05 | Mitsubishi Electric Corp | Airframe guiding apparatus |
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