JPH04127000A - Pilotless aircraft system - Google Patents
Pilotless aircraft systemInfo
- Publication number
- JPH04127000A JPH04127000A JP24839390A JP24839390A JPH04127000A JP H04127000 A JPH04127000 A JP H04127000A JP 24839390 A JP24839390 A JP 24839390A JP 24839390 A JP24839390 A JP 24839390A JP H04127000 A JPH04127000 A JP H04127000A
- Authority
- JP
- Japan
- Prior art keywords
- energy beam
- target
- controller
- ship
- water
- 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
- 239000000463 material Substances 0.000 claims description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 11
- 230000001678 irradiating effect Effects 0.000 abstract description 3
- 230000001902 propagating effect Effects 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 5
- 235000006506 Brasenia schreberi Nutrition 0.000 description 4
- 238000001514 detection method Methods 0.000 description 4
- 238000010304 firing Methods 0.000 description 3
- 238000007796 conventional method Methods 0.000 description 2
- 230000006378 damage Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/08—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles for carrying measuring instruments; Arrangements for mounting sensitive cargo within a projectile; Arrangements for acoustic sensitive cargo within a projectile
Abstract
Description
【発明の詳細な説明】
［産業上の利用分野１
この発明は、艦載回転翼機の捜索・探知情報に是つき、
水上艦艇から発射された直進するエネルキービー１１を
反射して曲進させることにより、水平線以遠の目標にエ
ネルギービームを照射し、破咳することをｌｊＪ能にす
る折り畳み式ミラーを有する無人飛行体システムに関す
るものである。[Detailed Description of the Invention] [Industrial Application Field 1] This invention relates to search and detection information for carrier-based rotary wing aircraft.
An unmanned aerial vehicle system with a folding mirror that enables ljj to irradiate energy beams to targets beyond the horizon by reflecting the straight-advancing Enerkibee 11 launched from a surface ship and causing it to go in a curved direction. It is related to.
１従来の技術］
従来は、水上艦艇からエネルギービームを発射しても、
直進するために、水平線以遠の目標に照射できないため
、水平線以遠の１−１標を破壊することができなかった
。1 Conventional technology] Conventionally, even if an energy beam was fired from a surface ship,
Because it was traveling straight, it was not possible to irradiate targets beyond the horizon, so it was not possible to destroy the 1-1 marker beyond the horizon.
従来の水−Ｌ−艦艇からのエネルギービーム発射の運用
概念を第３図に示す。Figure 3 shows the operational concept of energy beam firing from a conventional water-L-ship.
従来は、水上艦艇（」）のエネルギービーム発射機（５
）から発射されたエネルギービーム（２４）は、水平線
以内の水ト目標（２５）にしか照射されなかった。Conventionally, energy beam launchers (5
The energy beam (24) emitted from ) was only irradiated to the water target (25) within the horizon.
［発明か解決しようとする課題１
１−、ｉｉＸ！のように、従来の方法では、水平線以遠
の水」−目標にエネルギービームを照射てきないという
問題があった。[Invention or problem to be solved 1 1-, iiX! With conventional methods, there was a problem in that the energy beam could not be irradiated to the water target beyond the horizon.
この発明は、かかる欠点を抽除し、水・Ｆ線以遠の水−
に目標を捜索・探知し、直進する工不ルキービー１１を
曲進させて、水（ＩＺ線以遠の水１．１０：１つに１１
，６射てきるようにするＩＪ〒り畳み式ミラーを有する
無人飛行体システムを提供するものである。This invention eliminates such drawbacks and enables water-
Search and detect the target, make the Kofu Lukibee 11 go straight, make a turn, and search for water (water beyond the IZ line 1.10: 11 in one)
The present invention provides an unmanned aerial vehicle system having an IJ folding mirror that allows the IJ to fire at the aircraft.
１課題を解決するための手段１
この発明に関わる無人飛行体システムは、艦載回転翼機
の捜索センサの探知情報に基づく艦載回転翼機からの指
令により、水玉１工線以遠の水」二目標を追尾し、その
結果に姑つき制御される折り畳み式ミラーを用いるとと
もに、無人飛行体をホバーノングさせて、水上艦艇から
発射されたエネルギービームを反射曲進させて、水平線
以遠の水１′、［］（票（こ照射できるよう（こしたも
のである。1 Means for Solving the Problems 1 The unmanned aerial vehicle system according to the present invention is capable of detecting two targets, 1 and 2, by commands from a carrier-based rotary-wing aircraft based on detection information from a search sensor on the carrier-based rotary-wing aircraft. In addition to using a folding mirror that is controlled by tracking the results, the unmanned flying vehicle is made to hover, and the energy beam emitted from the surface ship is reflected and deflected, and the unmanned aircraft is able to fly beyond the horizon by 1', [ ] (This is a vote that can be irradiated.
１作用−１
この発明においては、水平線以遠の水−ｌｘ １−１標
を捜索・探知し、直進する水に艦艇から発射されたエネ
ルギービームを４反射曲進させて水平線以遠の水」−目
標に照射し、水１−目標を破壊することか可能である。1 Effect-1 In this invention, the water beyond the horizon is searched for and detected, and the energy beam emitted from the ship is reflected into the water that is moving straight ahead, and the energy beam is reflected back to the water beyond the horizon. It is possible to destroy the water target by irradiating it with water.
［実施例１
第１図は、この発明によるシステム構成図を、第２図は
、この発明による水−に艦艇からのエネルギービーム・
発射の運用概念を、各々示す。[Example 1] Fig. 1 shows a system configuration diagram according to the present invention, and Fig. 2 shows a system configuration diagram according to the present invention.
Each of the operational concepts of launch is shown.
艦載回転翼機（８）に装備される捜索センサ（１０）の
探知情報（］１）に基づく無人飛行体追尾管制装置（９
）からの指令信’３（１２）を、無人飛行体（１４）の
データリンク受信装置（１５）で受信の＋、その内容を
解読し、管制信号（１９）を追尾管制装置（１６）に伝
辻する。追尾管制装置（１６）は、水＼（Ｚ線以遠の水
上Ｉ；１標（２５）を追尾し、その結果に基つきホバー
リング装置（１７）にホバーリング信号（２０）を、姿
勢制御装置（１８）に制御信号（２Ｉ）を送出する１、
ホバーリング装置（１７）は、ホバーリング信号（２０
）に従い無人飛行体（１４）を所定の位置及び高度に占
位させる。姿勢制御装置（１８）は、制御信号（２１）
に従い折り畳み式ミラー（２２）にミラー制御信号（２
３）を送出し、折り畳み式ミラー（２２）を展開すると
ともに、所定の姿勢に設定する。Unmanned aerial vehicle tracking control device (9) based on detection information (]1) of a search sensor (10) installed on a carrier-based rotary wing aircraft (8)
) is received by the data link receiving device (15) of the unmanned aircraft (14), deciphers its contents, and transmits the control signal (19) to the tracking control device (16). Pass on. The tracking control device (16) tracks one mark (25) on water (water I beyond the Z line), and based on the result, sends a hovering signal (20) to the hovering device (17), and sends a hovering signal (20) to the attitude control device. 1 sending a control signal (2I) to (18);
The hovering device (17) sends a hovering signal (20
), the unmanned aerial vehicle (14) is positioned at a predetermined position and altitude. The attitude control device (18) receives a control signal (21)
Accordingly, the mirror control signal (2) is sent to the folding mirror (22).
3) is sent out, and the folding mirror (22) is unfolded and set to a predetermined posture.
艦」−システム（２）のエネルギービーム発射装置（４
）は、艦載回転翼機（８）の無人飛行体５６尾管制装置
（９）からの［Ｉ線情報（７）を受信した艦上追尾管制
装置（３）からの発射信号（６）を受けて、工不ルギー
ヒＡ発ＵＪｆｉ（５）からエネルギービーム（２４）ヲ
発射する。所定の位置及び姿勢に１投定された折り畳み
式ミラー（２２）は、工不ルキービー１−（２４）を反
射曲進させて、水平線以遠の水Ｉ−目標（２５）に照射
し水トロ標（２５）を破壊する。"Ship" - System (2) Energy Beam Launcher (4
) received the launch signal (6) from the carrier-based tracking control system (3) which received the I-line information (7) from the unmanned aerial vehicle 56 tail control system (9) of the carrier-based rotorcraft (8). , an energy beam (24) is fired from UJfi (5) from Kofurugihi A. The folding mirror (22), which is projected at a predetermined position and attitude, causes the engineering vehicle 1- (24) to move in a reflective curve and irradiates it to the water target (25) beyond the horizon. Destroy (25).
無人飛行体（１４）は、エネルギービーム（２４）によ
る破壊をさけるために、エネルギービーム（２４）を反
射拡散させるエネルギービーム・反射材料（＋３）で覆
われている。The unmanned aerial vehicle (14) is covered with an energy beam/reflective material (+3) that reflects and diffuses the energy beam (24) in order to avoid destruction by the energy beam (24).
［発明の効宋１
この発明は、以Ｉ−説明したとおり従来の方法てはてき
なかった。水・）Ｚ線以遠の水上目標を、捜索探知、追
尾し、水上艦艇から発射される工不ルキービーｌ＼て攻
撃することを１．＋Ｊ能とする。[Effects of the invention Song 1 This invention has not been achieved by conventional methods as explained below. 1. Searching, detecting, tracking, and attacking surface targets beyond the Z-line using watercraft fired from surface ships. +J Noh.
第１図はこの発明のシステト構成図、第２図はこの発明
の水上艦艇からのエネルギービーム発射の運用概念図、
第３図は従来の水」−艦艇からのエネルギービーム発射
の運用概念図である。
図において、（］）は］水上艦艇、２）は艦Ｉ〕システ
ム（３）は艦り追尾管制装置、（４）はエネルギービー
ム発射装置、（５）はエネルギービーム発射機、（６）
は発射信−７＃、（７）は目標情報、（８）は艦載回転
翼機、（９）は無人飛行体追尾管制装置、（１０）は捜
索センサ、 （Ｉ Ｉ）は探知情報、（＋２）は指令信
号、 （＋３）はエネルギービーム反射材料、 （＋４
）は無人飛行体、（＋５）はデータリンク受信装置、（
１，６）は追尾管制装置、 （＋７）はホバーリング装
置、（、＋８）は姿勢制御装置、（＋９）は管制信号（
２０）はポハーリング信吋、（２１）は制御信号、 （
２２）は折り畳み式ミラー、 （２３）はミラー制御信
冒’、（ｚ４）はエネルキービー１．．（２５）は水−
１ユｌＴ口：：Ｍ−Ｃ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
ている。Fig. 1 is a system configuration diagram of this invention, Fig. 2 is an operational conceptual diagram of energy beam firing from a surface ship of this invention,
Figure 3 is a conceptual diagram of the conventional operation of energy beam firing from a watercraft. In the figure, (]) is a surface ship, 2) is a ship I system, (3) is a ship tracking control system, (4) is an energy beam launcher, (5) is an energy beam launcher, and (6) is a ship tracking control system.
is the launch signal-7#, (7) is the target information, (8) is the carrier-based rotary wing aircraft, (9) is the unmanned aircraft tracking control system, (10) is the search sensor, (II) is the detection information, ( +2) is the command signal, (+3) is the energy beam reflecting material, (+4
) is an unmanned aerial vehicle, (+5) is a data link receiver, (
1, 6) is a tracking control device, (+7) is a hovering device, (, +8) is an attitude control device, (+9) is a control signal (
20) is the poharing signal, (21) is the control signal, (
22) is a folding mirror, (23) is a mirror control mirror, (z4) is an energy key bee 1. ．． (25) is water-
There is 1 unit T mouth::MC. In addition, the same or corresponding parts in the figures are given the same reference numerals.
Claims (1)
管制し、無人飛行体に正確にエネルギービームを発射す
る艦上システムと、水上目標を捜索するセンサを有し無
人飛行体を追尾管制する艦載回転翼機と、艦上システム
から発射されるエネルギービームを反射する凹面形状を
した折り畳み式ミラーと、折り畳み式ミラーを制御する
姿勢制御装置と、艦載回転翼機のセンサ情報に基づき水
平線以遠の水上目標を追尾・照準して、艦上システムか
ら発射されたエネルギービームを正確に追尾目標に照射
するために折り畳み式ミラーの姿勢制御装置を管制する
追尾管制装置と、艦載回転翼機からの管制信号を受信し
追尾管制装置に伝達するデータリンク受信装置と、ホバ
ーリング能力を有し、エネルギービーム反射材料で覆わ
れた無人飛行体で構成することを特徴とする無人飛行体
システム。Equipped on surface ships, it tracks and controls carrier-based rotorcraft and unmanned aerial vehicles, and has a shipboard system that accurately fires energy beams at unmanned aerial vehicles and sensors that search for surface targets. A carrier-based rotorcraft, a concave-shaped folding mirror that reflects the energy beam emitted from the carrier system, an attitude control device that controls the folding mirror, and a carrier-based rotary-wing aircraft based on sensor information from above the horizon. A tracking control device controls the attitude control device of the folding mirror in order to track and aim at the target and accurately irradiate the energy beam emitted from the shipboard system to the tracked target, and a control signal from the shipboard rotorcraft. An unmanned flying vehicle system comprising a data link receiving device that receives data and transmits the data to a tracking control device, and an unmanned flying vehicle that has hovering capability and is covered with an energy beam reflecting material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP24839390A JPH04127000A (en) | 1990-09-18 | 1990-09-18 | Pilotless aircraft system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP24839390A JPH04127000A (en) | 1990-09-18 | 1990-09-18 | Pilotless aircraft system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH04127000A true JPH04127000A (en) | 1992-04-27 |
Family
ID=17177444
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP24839390A Pending JPH04127000A (en) | 1990-09-18 | 1990-09-18 | Pilotless aircraft system |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH04127000A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100324581B1 (en) * | 1999-12-28 | 2002-02-16 | 박승창 | method for controlling of a pilotless airplane and apparatus for performming the same |
| JP2014126468A (en) * | 2012-12-26 | 2014-07-07 | Kawasaki Heavy Ind Ltd | Laser irradiation system using relay machine |
| US9887646B2 (en) | 2012-09-27 | 2018-02-06 | Shenzhen Byd Auto R&D Company Limited | Method for checking out-of-step of synchronous motor |
| US9887647B2 (en) | 2012-09-27 | 2018-02-06 | Shenzhen Byd Auto R&D Company Limited | Method for checking out-of-step of synchronous motor |
-
1990
- 1990-09-18 JP JP24839390A patent/JPH04127000A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100324581B1 (en) * | 1999-12-28 | 2002-02-16 | 박승창 | method for controlling of a pilotless airplane and apparatus for performming the same |
| US9887646B2 (en) | 2012-09-27 | 2018-02-06 | Shenzhen Byd Auto R&D Company Limited | Method for checking out-of-step of synchronous motor |
| US9887647B2 (en) | 2012-09-27 | 2018-02-06 | Shenzhen Byd Auto R&D Company Limited | Method for checking out-of-step of synchronous motor |
| JP2014126468A (en) * | 2012-12-26 | 2014-07-07 | Kawasaki Heavy Ind Ltd | Laser irradiation system using relay machine |
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