JPS63126792U - - Google Patents
Info
- Publication number
- JPS63126792U JPS63126792U JP1623987U JP1623987U JPS63126792U JP S63126792 U JPS63126792 U JP S63126792U JP 1623987 U JP1623987 U JP 1623987U JP 1623987 U JP1623987 U JP 1623987U JP S63126792 U JPS63126792 U JP S63126792U
- Authority
- JP
- Japan
- Prior art keywords
- antenna
- transmitter
- receiver
- circulator
- doppler
- 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
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
Description
第１図は、この考案の一実施例による電波ホー
ミング誘導弾のブロツク図、第２図は、従来の電
波ホーミングのブロツク図である。
図において１はアンテナ、２はサーキユレータ
、３は送信機、４は受信機、５はドツプラ検出器
、６は誘導計算部、７は操舵部、８はリア送信機
、９はリア受信機、１０はリアサーキユレータ、
１１はリアアンテナである。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てある。
FIG. 1 is a block diagram of a radio homing guided missile according to an embodiment of this invention, and FIG. 2 is a block diagram of conventional radio homing. In the figure, 1 is an antenna, 2 is a circulator, 3 is a transmitter, 4 is a receiver, 5 is a Doppler detector, 6 is a guidance calculation section, 7 is a steering section, 8 is a rear transmitter, 9 is a rear receiver, 10 is the rear circulator,
11 is a rear antenna. It should be noted that the same or corresponding parts in the drawings are designated by the same reference numerals.
Claims (1)
弾において、送信機と、サーキユレータと、アン
テナから出された電波を受信する受信機と、ドツ
プラ検出器の１出力をリアアンテナで送信するリ
ア送信機と、上記リアアンテナからの電波を受信
するリアサーキユレータと、リア受信機と、上記
ドツプラ検出器とリア受信機の両出力を入力する
誘導計算部と、操舵部とを備えた電波ホーミング
誘導弾。 A radio homing guided missile having a Doppler tracking function includes a transmitter, a circulator, a receiver that receives radio waves emitted from an antenna, a rear transmitter that transmits one output of the Doppler detector through a rear antenna, and the rear transmitter. A radio homing guided missile comprising a rear circulator that receives radio waves from an antenna, a rear receiver, a guidance calculation section that inputs the outputs of both the Doppler detector and the rear receiver, and a steering section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1623987U JPS63126792U (en) | 1987-02-06 | 1987-02-06 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1623987U JPS63126792U (en) | 1987-02-06 | 1987-02-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS63126792U true JPS63126792U (en) | 1988-08-18 |
Family
ID=30807913
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1623987U Pending JPS63126792U (en) | 1987-02-06 | 1987-02-06 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63126792U (en) |
-
1987
- 1987-02-06 JP JP1623987U patent/JPS63126792U/ja active Pending
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