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JPH0254912B2 - - Google Patents
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JPH0254912B2 - - Google Patents

Info

Publication number
JPH0254912B2
JPH0254912B2 JP58162821A JP16282183A JPH0254912B2 JP H0254912 B2 JPH0254912 B2 JP H0254912B2 JP 58162821 A JP58162821 A JP 58162821A JP 16282183 A JP16282183 A JP 16282183A JP H0254912 B2 JPH0254912 B2 JP H0254912B2
Authority
JP
Japan
Prior art keywords
signal
target
warhead
effective range
demodulator
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.)
Expired - Lifetime
Application number
JP58162821A
Other languages
Japanese (ja)
Other versions
JPS6053865A (en
Inventor
Osamu Saito
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP58162821A priority Critical patent/JPS6053865A/en
Publication of JPS6053865A publication Critical patent/JPS6053865A/en
Publication of JPH0254912B2 publication Critical patent/JPH0254912B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C13/00Proximity fuzes; Fuzes for remote detonation
    • F42C13/04Proximity fuzes; Fuzes for remote detonation operated by radio waves

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)

Description

【発明の詳細な説明】 〔発明の技術分野〕 この発明は、目標に送信波を照射し、目標から
の反射波を検知し、目標が誘導飛しよう体の近傍
を通過する時起爆パルスを発生する誘導飛しよう
体のアクテイブ近接信管に関するものである。
[Detailed Description of the Invention] [Technical Field of the Invention] This invention irradiates a target with a transmitted wave, detects a reflected wave from the target, and generates a detonation pulse when the target passes near a guided flying object. The invention relates to active proximity fuses for guided missiles.

〔従来技術〕[Prior art]

従来のこの種アクテイブ近接信管について簡単
に説明する。第1図において、Nはアクテイブ近
接信管、1は目標10に照射する送信波9のキヤ
リア信号を発生するキヤリア信号発生部、2はキ
ヤリア信号発生部1の出力のキヤリア信号を変調
し送信信号を発生すると同時に復調基準信号を発
生する送信信号発生部、3は送信信号発生部2の
出力の送信信号を増幅し高電力送信信号を出力す
る電力増幅器、4は電力増幅器3の出力の高電力
送信信号を2系統に分配する分配器、5は分配器
4により分配された高電力送信信号を上サイドア
ンテナ7に供給し、復調部A14、復調部B17
には供給せず、又、上サイドアンテナ7で受信し
た信号は復調部A14、復調部B17に供給し、
電力分配器4には供給しないサーキユレータ、6
は分配器4により分配された高電力送信信号を下
サイドアンテナ8に供給し、復調部A14、復調
部B17には供給せず、又、下サイドアンテナ8
で受信した信号は復調部A14、復調部B17に
供給し、電力分配器には供給しないサーキユレー
タ、7はサーキユレータ5より供給される高電力
送信信号を上側方向に照射し、目標10が上側近
傍通過時、目標10からの反射波11を受信する
上サイドアンテナ、8はサーキユレータ6より供
給される高電力送信信号を下側方向に照射し、目
標10が下側近傍通過時、目標10からの反射板
11を受信する下サイドアンテナ、9は上サイド
アンテナ7、下サイドアンテナ8より目標10に
照射される送信波、10はアクテイブ近接信管N
が検知する目標、11は目標10からの反射波、
12は送信信号発生部2の出力の復調基準信号に
より対地間探知距離を決定する対地ゲート信号を
発生するクラツタ間距離探知ゲート信号設定部で
あり、このクラツタ間距離探知ゲート信号設定部
は復調基準信号に探知ビーム方向の対地間距離に
相当する例えば次式に示す遅延時間だけ遅延させ
た(例えば復調基準信号の周波数に比例して遅延
時間が自動的に設定される) τC=Rc×2/150 τC……クラツタ遅延時間 Rc……探知ビーム方向の対地間距離対地ゲ
ート信号を発生する。13はクラツタ間距離探知
ゲート信号設定部12の出力の対地ゲート信号に
より目標探知距離を決定する目標ゲート信号を発
生する目標探知有効距離ゲート信号設定部であ
り、この目標探知有効距離ゲート信号設定部は対
地ゲート信号に探知ビーム方向の対地間距離に相
当する前式で示された遅延時間τCより次式に示
す通り所定の時間だけ遅延時間を短かくさせた τT=τC−τCO τT……目標遅延時間 τCO……クラツタ・目標弁別遅延時間目標ゲ
ート信号を発生する。14は上サイドアンテナ
7、下サイドアンテナ8で受信し、サーキユレー
タ5、サーキユレータ6を経由し供給される信号
とクラツタ間距離探知ゲート信号設定部12の出
力の対地ゲート信号より探知ビーム方向の対地間
距離が対地ゲート信号で設定している対地間距離
より短かくなるとサーキユレータより入力される
信号は対地ゲート信号により復調され短かくなつ
た分に比例したレベルの信号すなわちクラツタ復
調信号を発生する復調部A、15は復調部A14
の出力のクラツタ復調信号より対地間距離が、任
意に設定される弾頭有効距離に接近し侵入するこ
とを事前に検知し接近の程度及び侵入の程度によ
りすなわちクラツタ復調信号の出力レベルに応じ
て送信信号変調信号発生部16の例えば復調基準
信号の復調周波数を制御する制御信号を発生する
弾頭有効距離内クラツタ侵入検知回路、16は弾
頭有効距離内クラツタ侵入検知回路15の出力の
制御信号により例えば復調基準信号の変調周波数
を可変制御し、それにより送信信号発生部2で発
生する送信信号、及び、復調基準信号を制御する
変調基準信号を発生する送信信号変調信号発生
部、17は上サイドアンテナ7、下サイドアンテ
ナ8で受信し、サーキユレータ5、サーキユレー
タ6を経由し供給される信号と、目標探知有効距
離ゲート信号設定部13の出力の目標ゲート信号
より目標復調信号を発生する復調部B、18は復
調部B17の出力の目標復調信号より目標10迄
の距離が、その時設定されている目標探知距離よ
り外側にあるか内側にあるかを判断し、外側に存
在する場合はローレベル信号を、目標探知距離内
に侵入した場合はハイレベル信号を出力する目標
探知有効距離内目標侵入検知回路、19は目標探
知有効距離内目標侵入検知回路18の出力がハイ
レベル信号の場合起爆信号を発生し、ローレベル
信号の場合起爆信号を発生しない起爆信号検知回
路である。
A conventional active proximity fuse of this type will be briefly explained. In FIG. 1, N is an active proximity fuze, 1 is a carrier signal generator that generates a carrier signal of the transmission wave 9 to be irradiated to the target 10, and 2 is a carrier signal generator that modulates the carrier signal output from the carrier signal generator 1 to generate a transmission signal. 3 is a power amplifier that amplifies the transmit signal output from the transmit signal generator 2 and outputs a high power transmit signal; 4 is a high power transmitter for the output of the power amplifier 3; A divider 5 that divides the signal into two systems supplies the high power transmission signal distributed by the divider 4 to the upper side antenna 7, and includes a demodulator A14 and a demodulator B17.
The signal received by the upper side antenna 7 is not supplied to the demodulator A14, the demodulator B17,
A circulator that does not supply power to the power divider 4, 6
supplies the high power transmission signal distributed by the distributor 4 to the lower side antenna 8, does not supply it to the demodulator A14 and the demodulator B17, and also supplies the high power transmission signal distributed by the distributor 4 to the lower side antenna 8.
The signal received by the circulator 7 is supplied to the demodulator A14 and the demodulator B17, but not to the power divider.The circulator 7 irradiates the high power transmission signal supplied from the circulator 5 in an upward direction so that the target 10 passes near the upper side. When the target 10 passes near the lower side, the upper side antenna 8 receives the reflected wave 11 from the target 10 and radiates the high power transmission signal supplied from the circulator 6 downward. A lower side antenna receives the plate 11, 9 is a transmission wave irradiated to the target 10 from the upper side antenna 7 and the lower side antenna 8, 10 is an active proximity fuze N
is the target detected by , 11 is the reflected wave from target 10,
Reference numeral 12 denotes an inter-clutter distance detection gate signal setting unit that generates a ground gate signal for determining the ground-to-ground detection distance based on the demodulation reference signal output from the transmission signal generation unit 2; The signal is delayed by the delay time shown in the following formula, which corresponds to the ground distance in the direction of the detection beam (for example, the delay time is automatically set in proportion to the frequency of the demodulated reference signal) τC=Rc×2/ 150 τC...Clatsuta delay time Rc...Ground distance in the detection beam direction Generates a ground gate signal. Reference numeral 13 denotes a target detection effective range gate signal setting unit that generates a target gate signal for determining a target detection distance based on the ground gate signal output from the inter-clutter distance detection gate signal setting unit 12; τT = τC - τCO τT...Target Delay time τCO... Clutter/target discrimination delay time target gate signal is generated. 14 is a signal received by the upper side antenna 7 and lower side antenna 8 and supplied via the circulator 5 and circulator 6, and the ground gate signal output from the interclutter distance detection gate signal setting section 12. When the distance becomes shorter than the distance to the ground set by the ground gate signal, the signal input from the circulator is demodulated by the ground gate signal, and a demodulator generates a signal with a level proportional to the shortened distance, that is, a clutter demodulation signal. A, 15 is demodulation section A14
It is detected in advance that the distance between the ground approaches the arbitrarily set effective warhead distance and intrusion from the Kuratsuta demodulated signal output from the Kuratsuta demodulated signal. A warhead effective range clutter intrusion detection circuit 16 generates a control signal for controlling the demodulation frequency of the demodulation reference signal of the signal modulation signal generating section 16, and the warhead effective range clutter intrusion detection circuit 16 performs demodulation, for example, using a control signal output from the warhead effective range clutter intrusion detection circuit 15. 17 is an upper side antenna 7; a transmission signal modulation signal generation section that variably controls the modulation frequency of the reference signal and thereby generates a modulation reference signal that controls the transmission signal generated by the transmission signal generation section 2 and the demodulated reference signal; , a demodulation section B, 18 which generates a target demodulated signal from the signal received by the lower side antenna 8 and supplied via the circulator 5 and circulator 6, and the target gate signal output from the target detection effective range gate signal setting section 13. determines whether the distance to the target 10 is outside or inside the target detection distance set at that time from the target demodulated signal output from the demodulator B17, and if it is outside the target detection distance, outputs a low level signal. A target intrusion detection circuit within the target detection effective range outputs a high level signal when the target intrusion is within the target detection range, and 19 generates a detonation signal when the output of the target intrusion detection circuit 18 within the target detection effective range is a high level signal. , is a detonation signal detection circuit that does not generate a detonation signal in the case of a low level signal.

従来のアクテイブ近接信管Nは、上記の様に構
成され、目標10がアクテイブ近接信管Nの目標
探知有効距離内に侵入すると起爆信号が発生す
る。又、超低空時における、クラツタがアクテイ
ブ近接信管Nの弾頭有効距離内に侵入すると、ク
ラツタで起爆信号が発生してしまうため、クラツ
タ間距離程度により目標ゲート信号を制御し目標
探知有効距離を弾頭有効距離範囲内で可変するこ
とにより、クラツタで起爆信号が発生するのを防
止している。
The conventional active proximity fuse N is configured as described above, and when the target 10 enters within the target detection range of the active proximity fuse N, a detonation signal is generated. In addition, if a Kuratsuta enters within the warhead effective range of the active proximity fuze N at extremely low altitude, a detonation signal will be generated at the Kuratsuta, so the target gate signal is controlled depending on the distance between the Kuratsuta and the target detection effective range is adjusted to reduce the warhead's effective range. By varying the range within the effective distance range, it prevents the detonation signal from being generated by Kuratsuta.

しかるに、クラツタ間距離がアクテイブ近接信
管Nの弾頭有効距離内に侵入すると目標探知有効
距離が短かくなり、従つて、目標探知有効範囲が
急激に狭くなつてしまうという欠点があつた。
(誘導飛しよう体の目標10撃墜能力の低下。特
に近年は、低空目標に対する誘導飛しよう体の撃
墜能力の向上に対する要望が強く、上記欠点が重
要な課題となつている。) 〔発明の概要〕 この発明は、かかる欠点を改善する目的でなさ
れたもので、クラツタの影響を受ける下サイドア
ンテナの目標探知距離は従来通り処理し、クラツ
タの影響を受けない上サイドアンテナの目標探知
距離は、常に一定距離(弾頭有効距離)になる様
制御することにより、低空目標に対する目標探知
有効範囲が急激に狭くなることを防止し、誘導飛
しよう体の目標10撃墜能力を向上させるアクテ
イブ近接信管を提案するものである。
However, if the distance between the clutters enters the warhead effective range of the active proximity fuze N, the effective target detection range becomes short, and therefore the target detection effective range suddenly becomes narrower.
(Decrease in the ability of guided air vehicles to shoot down targets 10. Especially in recent years, there has been a strong desire to improve the ability of guided air vehicles to shoot down low-altitude targets, and the above drawbacks have become an important issue.) [Summary of the invention] ] This invention was made with the aim of improving this drawback.The target detection distance of the lower side antenna, which is affected by clutter, is processed as before, and the target detection distance of the upper side antenna, which is not affected by clutter, is We propose an active proximity fuze that prevents the effective target detection range for low-altitude targets from rapidly narrowing by controlling the warhead to always maintain a constant distance (effective warhead distance) and improves the ability of guided flying vehicles to shoot down 10 targets. It is something to do.

〔発明の概要〕[Summary of the invention]

第2図はこの発明の一実施例を示す図であり、
1〜4、6〜19は第1図と同じであり、5は従
来分配器4により分配された高電力送信信号を上
サイドアンテナ7に供給し、復調部A14及び復
調部B17には供給せず、又、上サイドアンテナ
7で受信した信号は、復調部A14及び復調B1
7に供給し、電力分配器4には供給しないサーキ
ユレータであるが、第2図では、分配器4により
分配された高電力送信信号を上サイドアンテナ7
に供給し、第1図に対して新たに付加した装置で
ある復調部C21には供給せず、又上サイドアン
テナ7で受信した信号は、復調部C21に供給
し、電力分配器4には供給しないサーキユレータ
で、20〜23が第1図に対して新たに付加した
装置である。20は、送信信号発生部2の出力の
復調基準信号により弾頭有効距離を常時一定に維
持する弾頭ゲート信号を発生する弾頭有効距離ゲ
ート信号設定部、21は上サイドアンテナ7で受
信し、サーキユレータ5を経由し供給される信号
と弾頭有効距離ゲート信号設定部20の出力の弾
頭ゲート信号より弾頭復調信号を発生する復調部
C、22は復調部C21の出力の弾頭復調信号よ
り目標10迄の距離が、常に一定に設定されてい
る弾頭有効距離より外側にあるか内側にあるかを
判断し、外側の場合はローレベル信号を、弾頭有
効距離内に侵入してきた時ハイレベル信号を出力
する弾頭有効距離内目標侵入検知回路、23は弾
頭有効距離内目標侵入検知回路22及び目標探知
有効距離内目標侵入検知回路18の出力が、どち
らもローレベル信号の場合、ローレベル信号を出
力し、それ以外の場合ハイレベル信号を出力する
OR回路である。
FIG. 2 is a diagram showing an embodiment of this invention,
1 to 4 and 6 to 19 are the same as in FIG. Furthermore, the signal received by the upper side antenna 7 is sent to the demodulator A14 and the demodulator B1.
In FIG. 2, the high power transmission signal distributed by the distributor 4 is sent to the upper side antenna 7.
The signal received by the upper side antenna 7 is supplied to the demodulator C21 and is not supplied to the demodulator C21, which is a newly added device in FIG. 20 to 23 are circulators that are not supplied, and are newly added devices to FIG. 20 is a warhead effective range gate signal setting unit that generates a warhead gate signal to keep the warhead effective range constant at all times using the demodulated reference signal output from the transmission signal generator 2; 21 is a signal received by the upper side antenna 7; The demodulation unit C, 22 generates a warhead demodulation signal from the warhead gate signal output from the warhead effective range gate signal setting unit 20 and the signal supplied via the warhead effective range gate signal setting unit 20. The warhead determines whether it is outside or inside the warhead's effective range, which is always set at a constant value, and outputs a low-level signal if it is outside, and a high-level signal when it enters within the warhead's effective range. The target intrusion detection circuit within effective range 23 outputs a low level signal when the outputs of the warhead effective range target intrusion detection circuit 22 and the target detection within effective range target intrusion detection circuit 18 are both low level signals. Outputs a high level signal in other cases
It is an OR circuit.

上記のように構成されたアクテイブ近接信管
N′においては、クラツタ間距離がアクテイブ近
接信管N′の弾頭有効距離内に侵入しても、下サ
イドアンテナ8の目標探知距離は、クラツタで起
爆信号が発生しない様にするため短かくなるが、
クラツタの影響を受けない上サイドアンテナ7の
目標探知距離は、常に弾頭有効距離を維持するこ
とになる。したがつて、目標探知有効範囲の急激
な低下が防止されることになる。
Active proximity fuze configured as above
At N', even if the distance between the clusters enters the warhead effective range of the active proximity fuze N', the target detection distance of the lower side antenna 8 will be shortened to prevent the detonation signal from being generated at the cluster. ,
The target detection range of the upper side antenna 7, which is not affected by clutter, always maintains the warhead effective range. Therefore, a sudden decrease in the target detection effective range is prevented.

〔発明の効果〕〔Effect of the invention〕

この発明は以上説明したとおりの構成により、
低空目標に対する目標探知有効範囲の低下を軽減
し、低空目標に対する、誘導飛しよう体の目標撃
墜能力を向上させるという効果がある。
This invention has the configuration as explained above,
This has the effect of reducing the reduction in the effective target detection range for low-altitude targets and improving the ability of guided flying vehicles to shoot down low-altitude targets.

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

第1図は従来のアクテイブ近接信管を示すブロ
ツク構成図、第2図はこの発明の一実施例を示す
ブロツク構成図である。 図において1はキヤリア信号発生部、2は送信
信号発生部、3は電力増幅器、4は電力分配器、
5はサーキユレータA、6はサーキユレータB、
7は上サイドアンテナ、8は下サイドアンテナ、
9は送信波、10は目標、11は反射波、12は
クラツタ間距離探知ゲート信号設定部、13は目
標探知有効距離ゲート信号設定部、14は復調部
A、15は弾頭有効距離内クラツタ侵入検知回
路、16は送信信号変調制御信号発生部、17は
復調部B、18は目標探知有効距離内目標侵入検
知回路、19は起爆信号発生回路、20は弾頭有
効距離ゲート信号設定部、21は復調部C、22
は弾頭有効距離内目標侵入検知回路、23はOR
回路、Nはアクテイブ近接信管である。なお、図
中同一符号は同一または相当部分を示すものとす
る。
FIG. 1 is a block diagram showing a conventional active proximity fuse, and FIG. 2 is a block diagram showing an embodiment of the present invention. In the figure, 1 is a carrier signal generator, 2 is a transmission signal generator, 3 is a power amplifier, 4 is a power divider,
5 is circulator A, 6 is circulator B,
7 is the upper side antenna, 8 is the lower side antenna,
9 is a transmitted wave, 10 is a target, 11 is a reflected wave, 12 is an inter-clutter distance detection gate signal setting section, 13 is a target detection effective range gate signal setting section, 14 is a demodulation section A, 15 is a clutter intrusion within the warhead effective range Detection circuit, 16 is a transmission signal modulation control signal generation section, 17 is a demodulation section B, 18 is a target detection effective range target intrusion detection circuit, 19 is a detonation signal generation circuit, 20 is a warhead effective range gate signal setting section, 21 is a Demodulator C, 22
is the warhead effective range target intrusion detection circuit, 23 is OR
The circuit, N, is an active proximity fuse. Note that the same reference numerals in the figures indicate the same or corresponding parts.

Claims (1)

【特許請求の範囲】[Claims] 1 目標に照射する送信波のキヤリア信号を発生
するキヤリア信号発生部と、キヤリア信号を変調
し送信信号を発生すると同時に復調基準信号を発
生する送信信号発生部と、送信信号を増幅し高電
力送信信号を出力する電力増幅器と、高電力送信
信号を上サイドアンテナと下サイドアンテナに分
配する電力分配器と、分配された高電力送信信号
を上サイドアンテナに供給し、復調部A、復調部
Bには供給せず、又、上サイドアンテナで受信し
た信号は復調部A、復調部Bに供給し、電力分配
器には供給しないサーキユレータAと、分配され
た高電力送信信号を下サイドアンテナに供給し、
復調部A、復調部Bには供給せず、又、下サイド
アンテナで受信した信号は、復調部A、復調部B
に供給し、電力分配器には供給しないサーキユレ
ータBと、供給された高電力送信信号を上側方向
に照射し、目標が上側近傍通過時、目標からの反
射波を受信する上サイドアンテナと、供給された
高電力送信信号を下側方向に照射し、目標が下側
近傍通過時、目標からの反射波を受信する下サイ
ドアンテナと、復調基準信号により対地間探知距
離を決定する対地ゲート信号を発生するクラツタ
間距離探知ゲート信号設定部と、対地ゲート信号
より目標探知距離を決定する目標ゲート信号を発
生する目標探知有効距離ゲート信号設定部と、反
射波と対地ゲート信号よりクラツタ復調信号を発
生する復調部Aと、クラツタ復調信号より対地間
距離が、弾頭有効距離に接近し侵入することを事
前に検知し、接近の程度及び侵入の程度により送
信信号変調信号を制御する制御信号を発生する弾
頭有効距離内クラツタ侵入検知回路と、弾頭有効
距離内クラツタ侵入検知回路の出力の制御信号に
より送信信号発生部を制御する変調基準信号を発
生する送信信号変調信号発生部と、反射波と目標
ゲート信号より目標復調信号を発生する復調部B
と、目標復調信号より目標までの距離が、その時
設定されている目標探知距離より外側にあるか内
側にあるかを判断し、外側の場合はローレベル信
号を、目標探知距離内に侵入してきた時ハイレベ
ル信号を出力する、目標探知有効距離内目標侵入
検知回路と、目標探知有効距離内目標侵入検知回
路の出力がハイレベル信号の場合起爆信号を発生
し、ローレベル信号の場合起爆信号を発生しない
起爆信号発生回路を備えた近接信管において、復
調基準信号により弾頭有効距離を常時一定に維持
する弾頭ゲート信号を発生する弾頭有効距離ゲー
ト信号設定部と、上サイドアンテナで受信する反
射波と弾頭ゲート信号より弾頭復調信号を発生す
る復調部Cと、弾頭復調信号より目標までの距離
が、常に一定に設定されている弾頭有効距離より
外側にあるか内側にあるかを判断し、外側の場合
はローレベル信号を、弾頭有効距離内に侵入して
きた時ハイレベル信号を出力する弾頭有効距離内
目標侵入検知回路と、弾頭有効距離内目標侵入検
知回路、又は、目標探知有効距離内目標侵入検知
回路の出力がハイレベル信号の場合、ハイレベル
信号を起爆信号発生回路へ供給し、それ以外の場
合はローレベル信号を起爆信号発生回路へ供給す
るOR回路を有したことを特徴とするアクテイブ
近接信管。
1. A carrier signal generation section that generates a carrier signal of a transmission wave to be irradiated to a target, a transmission signal generation section that modulates the carrier signal and generates a transmission signal and at the same time generates a demodulation reference signal, and amplifies the transmission signal and performs high-power transmission. A power amplifier that outputs a signal, a power divider that distributes a high power transmission signal to an upper side antenna and a lower side antenna, and a demodulation section A and a demodulation section B that supply the distributed high power transmission signal to the upper side antenna. Also, the signal received by the upper side antenna is supplied to demodulator A and demodulator B, but not to the power divider, and the distributed high power transmission signal is sent to the lower side antenna. supply,
The signal received by the lower side antenna is not supplied to demodulator A and demodulator B, and is not supplied to demodulator A and demodulator B.
a circulator B that supplies power to the power source and does not supply power to the power divider; an upper side antenna that irradiates the supplied high power transmission signal in an upward direction and receives reflected waves from the target when the target passes near the upper side; A lower side antenna receives the reflected wave from the target when the target passes near the lower side, and a ground gate signal that determines the ground detection distance using the demodulated reference signal. A clutter distance detection gate signal setting section that generates a clutter distance detection gate signal, a target detection effective range gate signal setting section that generates a target gate signal that determines the target detection distance from the ground gate signal, and a clutter demodulation signal from the reflected wave and the ground gate signal. The demodulator A detects in advance that the distance to the ground approaches the effective range of the warhead and intrudes from the Kuratsuta demodulated signal, and generates a control signal to control the transmission signal modulation signal depending on the degree of approach and the degree of intrusion. A warhead effective range clutter intrusion detection circuit, a transmission signal modulation signal generation section that generates a modulation reference signal that controls the transmission signal generation section using a control signal output from the warhead effective range clutter intrusion detection circuit, and a reflected wave and a target gate. Demodulator B generates a target demodulated signal from the signal
Then, based on the target demodulated signal, it is determined whether the distance to the target is outside or inside the target detection distance set at that time, and if it is outside, a low level signal is sent. When the output of the target intrusion detection circuit within target detection effective range outputs a high level signal and the output of the target intrusion detection circuit within target detection effective range is a high level signal, a detonation signal is generated, and when it is a low level signal, a detonation signal is generated. In a proximity fuze equipped with a detonation signal generation circuit that does not generate a detonation signal, a warhead effective range gate signal setting section that generates a warhead gate signal that constantly maintains a warhead effective range constant by a demodulated reference signal, and a reflected wave received by an upper side antenna. A demodulator C generates a warhead demodulation signal from a warhead gate signal, and a demodulator C determines from the warhead demodulation signal whether the distance to the target is outside or inside the warhead effective distance, which is always set to a constant value. A warhead within effective range target intrusion detection circuit outputs a low level signal when the warhead intrudes within the effective range, and a warhead target intrusion detection circuit outputs a high level signal when the warhead intrudes within the effective range. An active device characterized by having an OR circuit that supplies a high level signal to the detonation signal generation circuit when the output of the detection circuit is a high level signal, and otherwise supplies a low level signal to the detonation signal generation circuit. Proximity fuse.
JP58162821A 1983-09-05 1983-09-05 Active proximity fuse Granted JPS6053865A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58162821A JPS6053865A (en) 1983-09-05 1983-09-05 Active proximity fuse

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58162821A JPS6053865A (en) 1983-09-05 1983-09-05 Active proximity fuse

Publications (2)

Publication Number Publication Date
JPS6053865A JPS6053865A (en) 1985-03-27
JPH0254912B2 true JPH0254912B2 (en) 1990-11-22

Family

ID=15761865

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58162821A Granted JPS6053865A (en) 1983-09-05 1983-09-05 Active proximity fuse

Country Status (1)

Country Link
JP (1) JPS6053865A (en)

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4731170U (en) * 1971-04-24 1972-12-08
JPS51128199A (en) * 1975-04-30 1976-11-08 Tech Res & Dev Inst Of Japan Def Agency Proximity fuse

Also Published As

Publication number Publication date
JPS6053865A (en) 1985-03-27

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