JPH0254099U - - Google Patents

Info

Publication number
JPH0254099U
JPH0254099U JP12864888U JP12864888U JPH0254099U JP H0254099 U JPH0254099 U JP H0254099U JP 12864888 U JP12864888 U JP 12864888U JP 12864888 U JP12864888 U JP 12864888U JP H0254099 U JPH0254099 U JP H0254099U
Authority
JP
Japan
Prior art keywords
signal
return
target point
flying object
launch
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
JP12864888U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP12864888U priority Critical patent/JPH0254099U/ja
Publication of JPH0254099U publication Critical patent/JPH0254099U/ja
Pending legal-status Critical Current

Links

Description

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

第1図はこの考案の一実施例を示す構成ブロツ
ク図、第2図はa,b,cはこの考案の動作を示
す動作説明図、第3図は従来の飛しよう体を示す
構成ブロツク図、第4図a,b,cは従来の飛し
よう体の動作を示す動作説明図である。 図において、1は目標、2は発射装置、3は初
中期メモリ部、4は慣性誘導部、5はオートパイ
ロツト、6は操舵装置、7は制御信号発生装置、
8は電源、9は推進装置、10は発射機構作動装
置、11は小型爆弾発射機構、15は帰還復路メ
モリ部、16は切換器、17は帰還信号発生部、
Mは小型爆弾、Nは飛しよう体である。尚、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 configuration block diagram showing an embodiment of this invention, Fig. 2 is an explanatory diagram of a, b, and c showing the operation of this invention, and Fig. 3 is a configuration block diagram showing a conventional flying object. , FIGS. 4a, 4b, and 4c are operation explanatory diagrams showing the operation of a conventional flying object. In the figure, 1 is a target, 2 is a launcher, 3 is an early and intermediate memory section, 4 is an inertial guidance section, 5 is an autopilot, 6 is a steering device, 7 is a control signal generator,
8 is a power source, 9 is a propulsion device, 10 is a firing mechanism operating device, 11 is a small bomb firing mechanism, 15 is a return trip memory section, 16 is a switching device, 17 is a return signal generation section,
M is a small bomb and N is a flying object. In the drawings, the same or corresponding parts are denoted by the same reference numerals.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 飛しよう体が発射装置より発射されてから目標
地点に到達するまでの飛しよう経路をあらかじめ
記憶している飛しよう体の中の初中期メモリ部と
、現在飛しようしている飛しよう体の位置・速度
・方向を観測し誘導信号を出力する慣性誘導部と
、慣性誘導部より出力される誘導信号と初中期メ
モリ部より出力される初中期信号により飛しよう
体の飛しよう経路を修正し、目標地点に到達する
ために操舵指令信号を出力するオートパイロツト
と、飛しよう体の飛しよう経路を目標地点まで操
舵指令信号により操舵するための操舵装置と、初
中期信号と誘導信号により飛しよう体が目標地点
に到達したことを検知し、制御信号により発射機
構作動装置を制御する制御信号発生装置と、構成
品に必要な電力を供給する電源と、飛しよう体に
推力を与える推進装置と、制御信号により目標に
向つて小型爆弾を発射するための発射指令信号を
出力する発射機構動作装置と、発射指令信号によ
り飛しよう体が目標へ向つて小型爆弾を発射する
ための小型爆弾発射機構と、目標を撃破するため
の小型爆弾を備えた飛しよう体において、小型爆
弾を発射した後帰還するために、発射時かに目標
地点までの飛しよう経路を記憶している帰還復路
メモリ部と、発射時から目標地点へ飛しよう体の
飛しよう経路を操舵するための操舵指令信号を伝
送し帰還時は帰還信号により飛しよう体の飛しよ
う経路を操舵するため、操舵指令信号を伝送しな
いようにするための切換器と、制御信号と帰還復
路信号と誘導信号により、小型爆弾を発射後発射
装置へ帰還するための帰還信号を操舵装置へ出力
する帰還信号発生部とで構成したことを特徴とす
る飛しよう体。
An early and intermediate memory section within the flying object that stores in advance the flight path from when the flying object is launched from the launcher until it reaches the target point, and the current position of the flying object. - An inertial guidance section that observes the speed and direction and outputs a guidance signal, and a guidance signal output from the inertial guidance section and an initial/intermediate signal output from the initial/intermediate memory section to correct the flight path of the flying object. An autopilot outputs a steering command signal in order to reach the target point, a steering device uses the steering command signal to steer the flight path of the flying object to the target point, and an autopilot outputs a steering command signal to reach the target point. a control signal generator that detects that the aircraft has reached the target point and controls the launch mechanism operating device using control signals; a power source that supplies the necessary power to the components; and a propulsion device that provides thrust to the flying object. A launch mechanism operating device that outputs a launch command signal for launching a small bomb toward a target in response to a control signal, and a small bomb launch mechanism that causes a flying object to launch a small bomb toward a target in response to a launch command signal. , in a flying vehicle equipped with a small bomb for destroying a target, in order to return after firing the small bomb, a return trip memory section that stores the flight route to the target point at the time of firing; From the time of launch, a steering command signal is transmitted to steer the flight path of the object to the target point, and when returning, the return signal is used to steer the flight path of the object, so the steering command signal is not transmitted. and a return signal generator that outputs a return signal to the steering device to return the small bomb to the launcher after it has been launched, using a control signal, a return route signal, and a guidance signal. Let's fly.
JP12864888U 1988-09-30 1988-09-30 Pending JPH0254099U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12864888U JPH0254099U (en) 1988-09-30 1988-09-30

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12864888U JPH0254099U (en) 1988-09-30 1988-09-30

Publications (1)

Publication Number Publication Date
JPH0254099U true JPH0254099U (en) 1990-04-19

Family

ID=31382186

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12864888U Pending JPH0254099U (en) 1988-09-30 1988-09-30

Country Status (1)

Country Link
JP (1) JPH0254099U (en)

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