JPS5966171U - guided flying body - Google Patents
guided flying bodyInfo
- Publication number
- JPS5966171U JPS5966171U JP16251582U JP16251582U JPS5966171U JP S5966171 U JPS5966171 U JP S5966171U JP 16251582 U JP16251582 U JP 16251582U JP 16251582 U JP16251582 U JP 16251582U JP S5966171 U JPS5966171 U JP S5966171U
- Authority
- JP
- Japan
- Prior art keywords
- circuit
- amplifier
- antenna
- agc
- modulation
- 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)
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) [Abstract] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図は、従来の誘導飛しよう体の構成を示すブロック
図、第２図は、この考案の一実施例を示すブロック図で
あり、１は変調器、２はアンテナ、３は変調信号発生器
、４と９は増幅回路、６は復−調回路、６は検波回路、
７はＡＧＣ回路、８はアンテナ、１０はＡＧＣ補正回路
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 showing the configuration of a conventional guided flying object, and FIG. 2 is a block diagram showing an embodiment of this invention, in which 1 is a modulator, 2 is an antenna, and 3 is a modulated signal generator. 4 and 9 are amplifier circuits, 6 is a demodulation circuit, 6 is a detection circuit,
7 is an AGC circuit, 8 is an antenna, and 10 is an AGC correction circuit. In the drawings, the same or corresponding parts are designated by the same reference numerals.
Claims (1)
ｋＭ変調をかけるための変調器と、この変調器と復調回
路とにつながる変調信号発生回路と、上記第１のアンテ
ナと上記復調回路との間に設けられた第１の増幅回路と
、ＡＭ変調されていない受信信号を受信する第２のアン
テナと、上記第２のアンテナにつながる第２の増幅回路
と、第２の増幅器につながる検波回路と、この検波回路
につながり、その出力を第２の増幅器に与えるＡＧＣ回
路と、上記ＡＧＣ回路の出力端につながり自己の出力を
第１の増幅器に与えるＡＧＣ補正回路とを備えた誘導飛
しよう体。Located at the front of the first antenna, the angle of the control signal is A
A modulator for applying km modulation, a modulation signal generation circuit connected to the modulator and a demodulation circuit, a first amplifier circuit provided between the first antenna and the demodulation circuit, and an AM modulation circuit. a second antenna that receives a received signal that has not been detected; a second amplifier circuit connected to the second antenna; a detection circuit connected to the second amplifier; A guided flying object comprising an AGC circuit that supplies an amplifier to an amplifier, and an AGC correction circuit that is connected to an output end of the AGC circuit and supplies its own output to a first amplifier.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16251582U JPS5966171U (en) | 1982-10-27 | 1982-10-27 | guided flying body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16251582U JPS5966171U (en) | 1982-10-27 | 1982-10-27 | guided flying body |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5966171U true JPS5966171U (en) | 1984-05-02 |
Family
ID=30356850
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16251582U Pending JPS5966171U (en) | 1982-10-27 | 1982-10-27 | guided flying body |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5966171U (en) |
-
1982
- 1982-10-27 JP JP16251582U patent/JPS5966171U/en active Pending
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