JP2007078235A - Air defense system - Google Patents

Air defense system Download PDF

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JP2007078235A
JP2007078235A JP2005265649A JP2005265649A JP2007078235A JP 2007078235 A JP2007078235 A JP 2007078235A JP 2005265649 A JP2005265649 A JP 2005265649A JP 2005265649 A JP2005265649 A JP 2005265649A JP 2007078235 A JP2007078235 A JP 2007078235A
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air defense
uav
target
air
sensor
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JP4476910B2 (en
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Noriaki Kitahara
紀明 北原
Takeshi Shimamura
剛 島村
Mitsuyoshi Shinonaga
充良 篠永
Koji Oyama
晃司 大山
Makoto Soda
真 左右田
Hiroyuki Uemichi
裕之 上道
Takeshi Yasuda
武司 安田
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Toshiba Corp
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Toshiba Corp
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Abstract

<P>PROBLEM TO BE SOLVED: To provide an air defense system reinforced in a countermeasure to a threat target. <P>SOLUTION: This air defense system is constituted by loading a compact missile 20 capable of coping with an FB (Fighter Bomber) and a CM (Cruse Missile), on a UAV (unmanned Aerial Vehicle) 10. This system is generally put (equipped) on a defense line of a front line, and wirelessly remote-controls the UAV on the basis of target information from various aerial sensors such as a sensor-carrying aircraft and the like for the initial detection of an invading target. The missile loaded on the UAV attacks the threat target such as invading FBs, CMs and the like. <P>COPYRIGHT: (C)2007,JPO&INPIT

Description

この発明は防空システムに関する。   The present invention relates to an air defense system.

無人航空機システムとして例えば下記特許文献1、2に開示されるシステムが知られている。防空システムにおいて敵地を偵察する場合、有人航空機ではパイロット等への危険が大きいので、UAV(Unmanned Aerial Vehicle)と称する無人航空機を使用することが考えられている。
特開2005−28935号公報 特開2005−82018号公報
For example, systems disclosed in Patent Documents 1 and 2 below are known as unmanned aircraft systems. When scouting enemy territory in an air defense system, manned aircraft are highly dangerous to pilots and the like, and therefore it is considered to use unmanned aircraft called UAV (Unmanned Aerial Vehicle).
JP 2005-28935 A Japanese Patent Laid-Open No. 2005-82018

侵攻して来るFB(Fighter Bomber)やCM(Cruse Missile)等に対し洋上等で早期に迎撃する場合、航空基地から出撃するFI(Fighter Intercept)か、洋上等でCAP(Combat Air Patrol)しているFI、もしくは、洋上の艦船によって防空作戦を行うのが一般的である。このような防空システムの場合、日本を防衛するにあたっては十分な防衛策と言えず、日本の防衛は不十分と考えられる。
この発明は上記事情によりなされたもので、その目的は、脅威目標に対する対応を強化した防空システムを提供することにある。
When intercepting FB (Fighter Bomber), CM (Cruse Missile), etc. invading at an early stage on the ocean, perform FI (Fighter Intercept) from the air base or CAP (Combat Air Patrol) on the ocean. It is common to conduct air defense operations with existing FIs or offshore ships. In the case of such an air defense system, it cannot be said that it is a sufficient defensive measure to defend Japan, and Japan's defense is considered insufficient.
The present invention has been made under the circumstances described above, and an object of the present invention is to provide an air defense system with enhanced response to threat targets.

上記目的を達成するためにこの発明の一態様によれば、目標情報を取得するセンサと、脅威に対する防空処置を行う単一または複数の防空単位と、前記センサと前記防空単位との通信環境を形成する通信手段と、前記複数の防空単位のいずれかに属し、飛翔体を有する無人航空機とを具備し、前記センサにより取得された目標情報に基づいて、前記通信手段を介して前記無人航空機を操縦して前記飛翔体により脅威目標を迎撃するようにしたことを特徴とする防空システムが提供される。   In order to achieve the above object, according to one aspect of the present invention, there is provided a sensor for acquiring target information, a single or a plurality of air defense units for performing air defense measures against a threat, and a communication environment between the sensor and the air defense unit. Forming communication means, and an unmanned aerial vehicle belonging to one of the plurality of air defense units and having a flying object, the unmanned aircraft via the communication means based on the target information acquired by the sensor An air defense system is provided which is steered and intercepts a threat target by the flying object.

このような手段を講じることにより、例えばミサイルを搭載するUAVにより、様々な各種センサからの目標情報に基づいて侵攻してくるFBやCMなどへの対処を行うことができる。従って限られた目標情報しか得ることができない従来の防空システムの防空エリアよりも、より遠くで侵攻目標に対し対応/対処することが可能になる。   By taking such measures, for example, a UAV equipped with a missile can cope with invading FBs and CMs based on target information from various sensors. Accordingly, it is possible to respond / respond to the invasion target further away than the air defense area of the conventional air defense system that can obtain only limited target information.

この発明によれば、脅威目標に対する対応を強化した防空システムを提供することができる。   According to the present invention, it is possible to provide an air defense system with enhanced response to a threat target.

図1はこの発明に係わる防空システムの実施の形態を示すシステム図である。このシステムは例えば巡航ミサイルに対する地域防衛を目的として形成される。このシステムは地上に配備される、例えばSAMシステムのような防空システムを、飛行船100などのプラットフォームを介してリンクするようにしたものである。各防空システムはセンサを有し、脅威に対する防空処置を行う。   FIG. 1 is a system diagram showing an embodiment of an air defense system according to the present invention. This system is for example designed for regional defense against cruise missiles. In this system, an air defense system such as a SAM system deployed on the ground is linked via a platform such as an airship 100. Each air defense system has sensors and performs air defense measures against threats.

各防空システムに備わるシステム自体のセンサのみでは、遠距離から到来する、例えばFB1、CM2等の侵攻目標に関する目標情報を得ることができない場合がある。よって個々の防空システムにおいては限られた目標情報しか得られず脅威目標への対処が遅れる場合がある。そこでこの実施形態では、各センサからの目標情報について情報伝達型中継飛行船100を介して、地上に配備された防空システムに目標情報を分配、伝達することで、これまで対処が難しかった脅威目標に対し、対処可能となることを説明したものである。   In some cases, the target information related to the invasion target such as FB1, CM2, etc., which comes from a long distance, may not be obtained with only the sensor of the system itself provided in each air defense system. Therefore, in each air defense system, only limited target information can be obtained, and the response to the threat target may be delayed. Therefore, in this embodiment, the target information from each sensor is distributed and transmitted to the air defense system deployed on the ground via the information transmission type relay airship 100, so that it is difficult to deal with threat targets so far. On the other hand, it explains that it becomes possible to cope with it.

ところで、図1のシステムはFB1やCM2を対処できる小型ミサイルを搭載したUAV(滞空UAV、高速UAV)10を備える。そして、センサ搭載型航空機、地上に配備されるセンサ等のような、防衛ラインの最前線に配備される各種センサからの目標情報等を統合し、この統合目標情報に基づいてUAV10を侵攻目標まで素早く誘導する。さらに、その侵攻目標をUAV10に搭載したミサイルにより迎撃する。これにより既存の技術では十分な対処時間を確保できなかった脅威目標に対し、対処できるような防空システムを実現することができる。   By the way, the system of FIG. 1 is provided with a UAV (Aerial UAV, High Speed UAV) 10 equipped with a small missile capable of dealing with FB1 and CM2. Then, integrate target information from various sensors deployed on the forefront of the defense line, such as sensor-equipped aircraft, sensors deployed on the ground, etc. Guide quickly. Furthermore, the invasion target is intercepted by a missile mounted on the UAV10. As a result, it is possible to realize an air defense system that can deal with threat targets for which sufficient time cannot be secured with existing technology.

図2は、図1のシステムに用いられるUAVを示す概念図である。このUAV10は軽飛行機やグライダーなどにリモートコントロール機構を備えるようにしたもので、地上側システム、あるいは情報伝達型の飛行船、航空機を介して上空、または地上から無線操縦される。さらにこのUAV10は小型ミサイル20を搭載し、侵攻してくるFB、CM等の脅威目標を迎撃することができる。   FIG. 2 is a conceptual diagram showing a UAV used in the system of FIG. The UAV 10 includes a light aircraft, a glider, and the like equipped with a remote control mechanism, and is operated by radio from above or from the ground via a ground side system or an information transmission type airship or aircraft. Furthermore, this UAV 10 is equipped with a small missile 20 and can intercept threat targets such as FB and CM that are invading.

以上説明したようにこの実施形態では、UAV(Unmanned Aerial Vehicle)に、FB(Fighter Bomber)やCM(Cruse Missile)を対処可能な小型ミサイルを搭載する。そして、一般的に最前線の防衛ラインに配置(配備)され侵攻目標を初期探知するためのセンサ搭載型航空機等の各種空中センサからの目標情報をもとにUAVを無線により遠隔操縦する。そして、侵攻してくるFB、CM等の脅威目標を、UAVに搭載したミサイルで迎撃するようにする。これにより脅威目標に対して、既存の防空システムよりも、より遠くの位置から対応/対処することができるようになる。   As described above, in this embodiment, a small missile capable of dealing with FB (Fighter Bomber) and CM (Cruse Missile) is mounted on a UAV (Unmanned Aerial Vehicle). In general, the UAV is remotely operated by radio based on target information from various aerial sensors such as a sensor-equipped aircraft that is arranged (deployed) on the forefront defense line and initially detects an invasion target. Then, the invading FB, CM and other threat targets are intercepted by missiles installed in the UAV. As a result, the threat target can be dealt with / addressed from a farther position than the existing air defense system.

このように、既存の技術では限られたセンサからしか情報を得られない防空システム、構成品に対し、自システム以外からの目標情報を得て、侵攻してくるFB、CM等の脅威目標に対して小型ミサイルを搭載したUAVを防空システムの一部として使用することにより、より早く、より効率的に、より正確に、対応/対処できるようになる。また、このようなシステムを使用して日本国の防空システムにおける弱い部分を減少させることが可能になる。   In this way, for existing air defense systems and components that can only obtain information from limited sensors, target information from other than its own system is obtained for threat targets such as invading FBs and CMs. On the other hand, by using a UAV equipped with a small missile as part of an air defense system, it is possible to respond / treat faster, more efficiently and more accurately. Moreover, it becomes possible to reduce the weak part in a Japanese air defense system using such a system.

すなわちこの実施形態のように、各防空単位に保有する専用のセンサの情報を一元化して、CMやFB等を対処できる小型ミサイルを搭載したUAVを侵攻目標まで誘導して、FBやCM等の侵攻してくる脅威目標を対処することにより、限られた目標情報しか得ることができないような従来の防空システムよりも、より速く、より効率的に、より正確に、対応/対処できるような防空システムを構築することが可能となる。さらに、この様なシステムを構築することで、日本国の防空システムにおける脆弱な部分を減少させることが可能となる。   That is, as in this embodiment, the information of dedicated sensors held in each air defense unit is unified, and a UAV equipped with a small missile capable of dealing with CM, FB, etc. is guided to the invasion target, and FB, CM, etc. Air defense that can respond / respond faster, more efficiently and more accurately than traditional air defense systems that can only obtain limited target information by dealing with the invading threat target It becomes possible to construct a system. Furthermore, by building such a system, it is possible to reduce the fragile parts of Japan's air defense system.

なお、この発明は上記実施形態そのままに限定されるものではなく、実施段階ではその要旨を逸脱しない範囲で構成要素を変形して具体化できる。また、上記実施形態に開示されている複数の構成要素の適宜な組み合わせにより、種々の発明を形成できる。例えば、実施形態に示される全構成要素から幾つかの構成要素を削除、または幾つかの構成要素を追加してもよい。   Note that the present invention is not limited to the above-described embodiment as it is, and can be embodied by modifying the constituent elements without departing from the scope of the invention in the implementation stage. In addition, various inventions can be formed by appropriately combining a plurality of constituent elements disclosed in the embodiment. For example, some components may be deleted from some components shown in the embodiment, or some components may be added.

この発明に係わる防空システムの実施の形態を示すシステム図。The system figure which shows embodiment of the air defense system concerning this invention. 図1のシステムに用いられるUAVを示す概念図。The conceptual diagram which shows UAV used for the system of FIG.

符号の説明Explanation of symbols

10…UAV、20…小型ミサイル、1…FB、2…CM、100…飛行船   10 ... UAV, 20 ... small missile, 1 ... FB, 2 ... CM, 100 ... airship

Claims (2)

目標情報を取得するセンサと、
脅威に対する防空処置を行う単一または複数の防空単位と、
前記センサと前記防空単位との通信環境を形成する通信手段と、
前記複数の防空単位のいずれかに属し、飛翔体を有する無人航空機とを具備し、
前記センサにより取得された目標情報に基づいて、前記通信手段を介して前記無人航空機を操縦して前記飛翔体により脅威目標を迎撃するようにしたことを特徴とする防空システム。
A sensor for obtaining target information;
Single or multiple air defense units that provide air defenses against threats;
Communication means for forming a communication environment between the sensor and the air defense unit;
An unmanned aerial vehicle belonging to one of the plurality of air defense units and having a flying object,
An air defense system characterized in that, based on target information acquired by the sensor, the unmanned aircraft is operated via the communication means to intercept a threat target by the flying object.
前記センサは、防衛ラインの前線に配置され空中に任意の期間滞空する空中浮遊センサを含むことを特徴とする請求項1に記載の防空システム。 The air defense system according to claim 1, wherein the sensor includes an air floating sensor disposed on a front line of a defense line and staying in the air for an arbitrary period of time.
JP2005265649A 2005-09-13 2005-09-13 Air defense system Active JP4476910B2 (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101243044B1 (en) 2011-04-05 2013-03-18 대한민국 A target for fire training of portable guided missile
CN104309806A (en) * 2014-10-08 2015-01-28 中国航空工业集团公司西安飞机设计研究所 Cruise missile carrier vehicle
JP6097448B1 (en) * 2015-05-13 2017-03-15 株式会社 スカイロボット Color ball launcher
US10558218B2 (en) 2016-01-28 2020-02-11 Fujitsu Ten Limited Vehicle surroundings monitoring apparatus, monitoring system, remote monitoring apparatus, and monitoring method
CN110986680A (en) * 2019-10-12 2020-04-10 中国人民解放军国防科技大学 Composite interception method for low-speed small targets in urban environment
WO2020075407A1 (en) 2018-10-12 2020-04-16 三菱重工業株式会社 Flight body and flight body system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101243044B1 (en) 2011-04-05 2013-03-18 대한민국 A target for fire training of portable guided missile
CN104309806A (en) * 2014-10-08 2015-01-28 中国航空工业集团公司西安飞机设计研究所 Cruise missile carrier vehicle
JP6097448B1 (en) * 2015-05-13 2017-03-15 株式会社 スカイロボット Color ball launcher
US10558218B2 (en) 2016-01-28 2020-02-11 Fujitsu Ten Limited Vehicle surroundings monitoring apparatus, monitoring system, remote monitoring apparatus, and monitoring method
WO2020075407A1 (en) 2018-10-12 2020-04-16 三菱重工業株式会社 Flight body and flight body system
CN110986680A (en) * 2019-10-12 2020-04-10 中国人民解放军国防科技大学 Composite interception method for low-speed small targets in urban environment
CN110986680B (en) * 2019-10-12 2022-05-20 中国人民解放军国防科技大学 Composite interception method for low-speed small targets in urban environment

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