JPS5921997A - Warship guided missile - Google Patents

Warship guided missile

Info

Publication number
JPS5921997A
JPS5921997A JP57129874A JP12987482A JPS5921997A JP S5921997 A JPS5921997 A JP S5921997A JP 57129874 A JP57129874 A JP 57129874A JP 12987482 A JP12987482 A JP 12987482A JP S5921997 A JPS5921997 A JP S5921997A
Authority
JP
Japan
Prior art keywords
target
detection unit
barrage
error signal
guided missile
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
JP57129874A
Other languages
Japanese (ja)
Inventor
修 齋藤
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 JP57129874A priority Critical patent/JPS5921997A/en
Publication of JPS5921997A publication Critical patent/JPS5921997A/en
Pending legal-status Critical Current

Links

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

【発明の詳細な説明】 この発明は、目標から生ずる赤外線あるいは反射信号を
検知し、目標を捕捉、追尾する対艦誘導弾に関するもの
である。まず、従来のとの禎対鑑誘導弾(M)について
簡単に説明する。第1図において、山は対艦誘導弾(M
)が捕捉、追尾する目標。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an anti-ship guided missile that detects infrared rays or reflected signals generated from a target, and captures and tracks the target. First, the conventional guided missile (M) will be briefly explained. In Figure 1, the mountain is an anti-ship guided missile (M
) is acquired and tracked by the target.

+21 V′i目標山がら生ずる赤外線あるいは反射1
g号(以下信号と総称する)、+31は目標(1)から
の信号?受信する検知部、(4)は検知部(3)で受信
した信号から、誤羞信号七取9出す受信装置、(5)に
受信装置f4+の出力の誤差信号に1って検知部+37
 k目標からの信号(2)の到来方向に駆動する検知部
サーボ装置。
+21 V'i Infrared rays or reflections generated from the target mountain 1
Is No. g (hereinafter collectively referred to as signal), +31 a signal from target (1)? (4) is a receiving device that outputs an erroneous fear signal from the signal received by the detecting portion (3); (5) is a receiving device that outputs an error signal of the output of the receiving device f4+ by 1 and the detecting portion +37
k A detection unit servo device that is driven in the direction of arrival of the signal (2) from the target.

(6)は受信装置t +41の出力の誤差信号によって
機体を目標との会合点方向に操舵する操舵装置、(7)
は対艦誘導弾(M)に推力を与えるロケットモータであ
る。従来の、対!!誘導弾(M)に以上のaVC構成さ
れ、目標を捕捉し、その機体全目標との会合点へと訪導
し最終的に目標全撃破することを目的としている。
(6) is a steering device that steers the aircraft in the direction of the meeting point with the target using the error signal output from the receiving device t+41; (7)
is a rocket motor that provides thrust to anti-ship guided missiles (M). Conventional vs! ! The guided missile (M) is configured with the above aVC, and its purpose is to capture a target, guide the aircraft to the meeting point with all targets, and ultimately destroy all targets.

しかしながら、従来の対鑑誘4弾では、第2図に示す通
シの速度特性(VJ全金持ているため、目標と会合する
時間とは無関係に速度が一定である。
However, in the conventional 4 bullets, the speed characteristics of the pass shown in FIG.

従って、終末時の目標の急激[壇速した特等ンに対し追
随でもなくなったり、目標艦船からの砲弾攻撃(弾幕)
によシ撃墜されたりして、目agA墜H目カに支障をも
たしていた。特に、近年I/′i艦船の高速化、各撞速
射砲を装備する傾向が強く、上記欠点が重要な課題とな
っている。
Therefore, at the end of the day, the target's sudden attack [such as a sudden attack by a special ship that can no longer follow the target, or a cannonball attack (barrage) from the target ship.
He was often shot down, which caused problems with his ability to shoot down. In particular, in recent years there has been a strong tendency for I/'i ships to increase in speed and to be equipped with rapid-firing guns, making the above-mentioned drawbacks an important issue.

この元明は、上記欠点金改讐する半金特徴としたもので
、受信装置(4)の出力全後述する新たVceけた構成
要素に入力し、d4の終末時に目標が急激な回避運動を
開始したり、砲弾攻撃全開始したとき速度特性(VJk
補正し、会合点において所定の追随特性が得られるよう
にすると同時に、目標防空網突破能カケ鍋めることVc
jす、目標撃破能力全向上させたものである。以下、こ
の兄明の誘導弾(M)VCついての具体列である第3図
を用いて説明する。
This Genmei is a half-metal feature that corrects the above-mentioned drawback, and the entire output of the receiving device (4) is input to a new Vce component, which will be described later, and at the end of d4, the target starts a sudden avoidance movement. or the speed characteristics (VJk
At the same time, the ability to break through the target air defense network is improved.Vc
The ability to destroy targets has been completely improved. Hereinafter, explanation will be given with reference to FIG. 3, which is a specific sequence of this brother Akira's guided missile (M) VC.

第3図において、(11〜(7)は第1図と同じである
In FIG. 3, (11 to (7)) are the same as in FIG.

(8)〜02Iが第1図に対し新之に付方tl t、た
装置で、(8)は受信装置(4)の出力により目標迄の
会合時間を計算し、設定された倫合時間前の任意の期間
+TJハイレベル信号信号力出力それ以外の時はローレ
ベル信号音出力する作動期間設定回路、 +91tま、
受信装置(4)の出力の誤差信号がIgr定のレベル以
上の時ノ・イレベル信号ケ出力し、I′JJT定のレベ
ル以下の時ローレベル信号を出力する誤差信号スレツン
ユホールド回路、 101は、目標力・らの砲弾の弾幕
音を検知し検知し^後は−・イレベル信号を出力し、検
知前はローレベル信号を出力する弾幕音検知部、 1u
llは作動期間設定回路(8)及び誤差信号スレツンユ
ホールド回路(9)の出力がノへイレベル信号會出力し
ているか、又は1作動期間設定回路(8)及び弾 音検
知部叫の出力がハイレベル信号を出力している時に補助
推進装置O4を作動させる補助推進装置制御回路、 (
12+は、補助推進装置制御回路tillの出力[工り
対鑑誘4弾の速度全増加させるための補助推進装置であ
る。
(8) to 02I are the devices that were attached to the new one in Figure 1, and (8) calculates the meeting time to the target based on the output of the receiving device (4), and calculates the meeting time that has been set. Operation period setting circuit that outputs a low level signal sound during any previous period + TJ high level signal signal power output, +91t,
Error signal thread hold circuit which outputs a low level signal when the error signal of the output of the receiving device (4) is above the level of Igr constant, and outputs a low level signal when it is below the level of I'JJT constant, 101 is a barrage sound detection unit that detects and detects the barrage sound of a cannonball with a target force, then outputs a low level signal, and outputs a low level signal before detection, 1u
ll indicates whether the output of the operation period setting circuit (8) and the error signal thread hold circuit (9) is outputting a low level signal, or the output of the operation period setting circuit (8) and the bullet sound detection section. an auxiliary propulsion device control circuit that operates the auxiliary propulsion device O4 when outputting a high-level signal;
12+ is an auxiliary propulsion device for completely increasing the speed of the auxiliary propulsion device control circuit TILL [Engineered Comparison Bullet 4].

この祐明は0以上の工うに構成されているため。This Yumei is composed of 0 or more units.

対艦誘導弾は誘導の終末時に目標が急激な回避運動を開
始し九シ、砲弾攻撃を開始すると、誘導弾の速度特性(
V)は第4図に示す通シ抽正σれる。それによって、対
′&誘導弾の目標値能力?同上させることが出来る。な
お、実施例においては、(8)〜u21iそれぞれ独立
した回路で示しているが、これを(8)〜u21の機能
?備えた1つの構成要素に置き候えてもよいことf’l
 Kうまでもない。
At the end of the guided anti-ship missile, the target begins a rapid evasive movement, and when the shell attack begins, the speed characteristics of the guided missile (
V) is given by the general abstraction σ shown in FIG. By that, target value ability of anti- & guided missile? Same as above. In the embodiment, (8) to u21i are each shown as an independent circuit, but this is the function of (8) to u21? f'l may be substituted with one component provided.
K. Of course.

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

第1図11″i′従来における対艦誘導弾の構成?示す
図、第2図は従来の対鑑誘4弾の4度%性を示す図、第
3図はこの元明による対艦誘導弾の構成例全示す図、第
4図はこの兄明の対艦誘導弾の速贋特性ケ示す図であり
2図中はlr1目標、 +2)Fi目標からの16号、
(3)は検知部、 +41tま受信装置、(5)は検知
部サーボ装置、 +611−を操舵装置、(7)はロケ
ットモータ、 181rよ作動期間設定回路、(9)は
誤差信号スレッシュホール1回路、uO)は弾幕音検知
部、uDは?iM助推進装置制@回路、u21II′i
補助推進装置、  (M)は対艦誘導弾、(V)はノ*
度特性Vである。 なお0図中同一あるいは相当部分には同−符号金付して
示しである。
Figure 1 shows the structure of a conventional anti-ship guided missile. Figure 2 shows the 4 degree % characteristic of the conventional anti-ship missile. Figure 3 shows the anti-ship guided missile by Genmei. Figure 4 is a diagram showing all examples of bullet configurations, and Figure 4 is a diagram showing the speed and counterfeit characteristics of this brother Akira's anti-ship guided missile.
(3) is the detection unit, +41t is the receiving device, (5) is the detection unit servo device, +611- is the steering device, (7) is the rocket motor, 181r is the operation period setting circuit, (9) is the error signal threshold 1 circuit, uO) is the barrage sound detection section, uD is? iM auxiliary propulsion system @circuit, u21II'i
Auxiliary propulsion system, (M) is anti-ship guided missile, (V) is *
This is the degree characteristic V. In Figure 0, the same or corresponding parts are designated with the same reference numerals.

Claims (1)

【特許請求の範囲】[Claims] 目標から生ずる赤外線あるいは反射信号を受信する検知
部と、この検知部で受信し比信号から誤差信号を取シ出
す受信装置と、受信装置の出力により検知部全目標方向
に駆動する検知部サーボ装置と、@体音目標との会合点
方向に操舵する操舵装置、推力金与えるロケットモータ
と?備え之誘導弾において9作動期間を設定する作動期
間設定回路と、目標が回避運動をし7を場合誤差信号が
増大するのを検知する誤差信号スレッシュホールド回路
と、目標からの砲弾の弾幕Mを検知する弾幕音検知部と
、補助4fB進装置の作動上制御する抽助推進装M制両
回路と、速度を増加させるための補助推進装置とを有す
ること全特徴とする誘導弾。
A detection unit that receives infrared rays or reflected signals generated from the target, a reception device that extracts an error signal from the ratio signal received by this detection unit, and a detection unit servo device that drives the detection unit in all target directions by the output of the reception device. And a steering device that steers the body in the direction of the meeting point with the target, a rocket motor that provides thrust? An activation period setting circuit that sets an activation period of 9 for prepared guided missiles, an error signal threshold circuit that detects an increase in the error signal when the target makes an evasive movement, and a barrage M of shells from the target. A guided missile having a barrage sound detection unit for detecting barrage sound, an extraction propulsion system M control circuit for controlling the operation of an auxiliary 4fB propulsion device, and an auxiliary propulsion device for increasing speed.
JP57129874A 1982-07-26 1982-07-26 Warship guided missile Pending JPS5921997A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57129874A JPS5921997A (en) 1982-07-26 1982-07-26 Warship guided missile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57129874A JPS5921997A (en) 1982-07-26 1982-07-26 Warship guided missile

Publications (1)

Publication Number Publication Date
JPS5921997A true JPS5921997A (en) 1984-02-04

Family

ID=15020438

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57129874A Pending JPS5921997A (en) 1982-07-26 1982-07-26 Warship guided missile

Country Status (1)

Country Link
JP (1) JPS5921997A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60216199A (en) * 1984-04-12 1985-10-29 三菱電機株式会社 Antiship guided missile
JPH0237297A (en) * 1988-07-28 1990-02-07 Mitsubishi Electric Corp Control device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50127396A (en) * 1974-03-27 1975-10-07
JPS58198700A (en) * 1982-05-14 1983-11-18 三菱電機株式会社 Guided missile

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50127396A (en) * 1974-03-27 1975-10-07
JPS58198700A (en) * 1982-05-14 1983-11-18 三菱電機株式会社 Guided missile

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60216199A (en) * 1984-04-12 1985-10-29 三菱電機株式会社 Antiship guided missile
JPH0237297A (en) * 1988-07-28 1990-02-07 Mitsubishi Electric Corp Control device

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