JPWO2020142121A5 - - Google Patents

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JPWO2020142121A5
JPWO2020142121A5 JP2021517608A JP2021517608A JPWO2020142121A5 JP WO2020142121 A5 JPWO2020142121 A5 JP WO2020142121A5 JP 2021517608 A JP2021517608 A JP 2021517608A JP 2021517608 A JP2021517608 A JP 2021517608A JP WO2020142121 A5 JPWO2020142121 A5 JP WO2020142121A5
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projectile
counterattack
uav
aircraft
target aircraft
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Priority claimed from US16/151,307 external-priority patent/US11440656B2/en
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対象航空機を無力化するシステムであって、
発射体発射機構と、
前記発射体発射機構により発射可能な発射体と、
飛行中の対象航空機を検出するように作動可能な少なくとも一つの検出センサを有する航空機検出システムであって、該航空機検出システムは、前記対象航空機の無力化を容易にするため、前記検出に応答して、前記発射機構または反撃無人航空機（UAV）の少なくとも一つにコマンドデータを提供するように作動可能であり、前記反撃UAVは、前記発射体に支持され、前記発射体から分離可能であり、航空機対抗手段を有する、航空機検出システムと、
を有し、
前記発射体は、相互に放出可能に結合された、前記反撃UAVを備える内側チャンバを定める、少なくとも第1のハウジング区画および第2のハウジング区画から形成され、
前記コマンドデータに基づき、前記発射体発射機構は、前記発射体を発射するように作動され、
前記第1のハウジング区画および前記第2のハウジング区画は、相互に分離可能であり、前記コマンドデータに基づき、前記対象航空機に対する所定の位置で、前記内側チャンバから前記反撃UAVが放出され、
前記発射体からの分離の際に、前記反撃UAVは、前記航空機対抗手段により、前記対象航空機を無力化するように作動される、システム。 A system for neutralizing a target aircraft, comprising:
a projectile launching mechanism;
a projectile launchable by the projectile launching mechanism;
An aircraft detection system having at least one detection sensor operable to detect a target aircraft in flight, the aircraft detection system responding to the detection to facilitate neutralization of the target aircraft. operable to provide command data to at least one of said launch mechanism or a counterattack unmanned aerial vehicle (UAV), said counterattack UAV supported by and separable from said projectile; an aircraft detection system having an aircraft countermeasure;
has
said projectile is formed from at least a first housing compartment and a second housing compartment releasably coupled to each other defining an inner chamber containing said counterattack UAV;
based on the command data, the projectile launching mechanism is activated to fire the projectile;
said first housing compartment and said second housing compartment being separable from each other, said counterattack UAV being ejected from said inner chamber at a predetermined position relative to said target aircraft based on said command data;
The system of claim 1, wherein upon separation from the projectile, the counterattack UAV is activated by the air countermeasures to neutralize the target aircraft. 前記反撃UAVは、予め定められた配置に前記反撃UAVを航空輸送するため、前記発射体内に折り畳まれた配置で構成され、
前記反撃UAVは、前記発射体からの分離の際に、広げられた位置に移動するように作動される、請求項1に記載のシステム。 said counterattack UAV configured in a folded configuration within said projectile for air transporting said counterattack UAV to a predetermined configuration;
3. The system of claim 1, wherein the counterattack UAV is actuated to move to a spread position upon separation from the projectile. 前記反撃UAVが前記発射体から放出される所定の位置は、前記対象航空機に対する空中位置を含み、前記反撃UAVは、前記対象航空機のセンサでは検出されない、請求項1に記載のシステム。 2. The system of claim 1 , wherein the predetermined location from which the counterattack UAV is emitted from the projectile includes an airborne location relative to the target aircraft, and wherein the counterattack UAV is not detected by sensors on the target aircraft. 前記コマンドデータは、妨害データ、航空機捕獲対抗手段配備コマンドデータ、対象航空機検出データ、反撃UAV制御データ、またはこれらの組み合わせの少なくとも一つを有する、請求項1に記載のシステム。 2. The system of claim 1 , wherein the command data comprises at least one of jamming data, aircraft capture countermeasure deployment command data, target aircraft detection data, counterattack UAV control data, or combinations thereof. 前記航空機検出システムは、前記反撃UAVにより支持された前記少なくとも一つの検出センサを有する、オンボード航空機検出システムを有し、
前記少なくとも一つの検出センサは、前記対象航空機の位置を検出するように構成され、
前記反撃UAVのフライト制御システムは、前記対象航空機の前記検出された位置に基づいて、前記反撃UAVの自動飛行を制御するように作動される、請求項1に記載のシステム。 the aircraft detection system comprises an on-board aircraft detection system comprising the at least one detection sensor carried by the counterattack UAV;
the at least one detection sensor is configured to detect the position of the target aircraft;
2. The system of claim 1 , wherein the counterattack UAV flight control system is operated to control automatic flight of the counterattack UAV based on the detected position of the target aircraft. 前記航空機検出システムは、前記発射体発射機構により支持された前記少なくとも一つの検出センサを有するオンプラットフォーム航空機検出システムを有し、
前記少なくとも一つの検出センサは、前記対象航空機を検出するように作動され、
前記オンプラットフォーム航空機検出システムは、前記反撃UAVにコマンドデータを提供し、前記対象航空機の妨害および無力化を容易化するように構成される、請求項1に記載のシステム。 the aircraft detection system comprises an on-platform aircraft detection system having the at least one detection sensor supported by the projectile launch mechanism;
the at least one detection sensor is activated to detect the target aircraft;
2. The system of claim 1 , wherein the on-platform aircraft detection system is configured to provide command data to the counterattack UAV to facilitate jamming and neutralization of the target aircraft. 前記航空機検出システムは、地上基地構造に関連する地上基地外部航空機検出システムを有し、
前記地上基地外部航空機検出システムは、前記対象航空機を検出するように作動される前記少なくとも一つの検出センサを有し、
前記地上基地外部航空機検出システムは、前記発射体発射機構または前記反撃UAVの少なくとも一つに、コマンドデータを提供し、前記対象航空機の妨害および無力化が容易化されるように作動される、請求項1に記載のシステム。 the aircraft detection system comprises a ground station external aircraft detection system associated with a ground station structure;
the ground-based external aircraft detection system having the at least one detection sensor actuated to detect the target aircraft;
wherein said ground-based external aircraft detection system provides command data to at least one of said projectile launcher or said counterattack UAV and is activated such that jamming and neutralization of said target aircraft is facilitated; The system of paragraph 1 . 前記反撃UAVは、飛行本体と、複数のロータ組立体とを有し、ロータ組立体の各々は、前記飛行本体の近傍に折り畳まれ、
前記複数のロータ組立体は、前記反撃UAVが前記発射体から分離された際に、前記飛行本体から広がるように構成される、請求項1に記載のシステム。 the counterattack UAV having a flight body and a plurality of rotor assemblies, each rotor assembly being folded about the flight body;
2. The system of claim 1, wherein the plurality of rotor assemblies are configured to spread out from the flight body when the counterattack UAV is separated from the projectile . 前記内側チャンバは、前記反撃UAVを折り畳まれた配置で収容する、請求項1に記載のシステム。 2. The system of claim 1 , wherein the inner chamber accommodates the counterattack UAV in a folded configuration . 前記発射体は、さらに、ハウジングリリース機構を有し、該ハウジングリリース機構は、前記第2のハウジング区画から前記第1のハウジング区画を少なくとも部分的に分離するように構成され、
前記内側チャンバが露出され、これにより、前記発射体からの前記反撃UAVの分離および放出が容易化される、請求項9に記載のシステム。 the projectile further comprising a housing release mechanism configured to at least partially separate the first housing compartment from the second housing compartment;
10. The system of claim 9 , wherein the inner chamber is exposed, thereby facilitating separation and ejection of the counterattack UAV from the projectile. 前記ハウジングリリース機構は、前記発射体と前記発射体発射機構の間に延在するテザーを有し、
前記発射体の発射の後、前記テザーは、前記第2のハウジング区画からの前記第1のハウジング区画の分離を促進し、前記発射体からの前記反撃UAVの分離および放出が容易化される、請求項10に記載のシステム。 the housing release mechanism has a tether extending between the projectile and the projectile launching mechanism;
after launch of the projectile, the tether facilitates separation of the first housing compartment from the second housing compartment to facilitate separation and ejection of the counterattack UAV from the projectile; 11. System according to claim 10 . 前記航空機対抗手段は、前記対象航空機の動作を妨害するように構成され、可撓性絡まり素子、ネット、流体、ペレット、放電装置、または照射装置の少なくとも一つを有する、請求項1に記載のシステム。 2. The aircraft countermeasures of claim 1, wherein the aircraft countermeasures are configured to interfere with the movement of the target aircraft and comprise at least one of flexible entanglement elements, nets, fluids, pellets, electrical discharge devices, or irradiation devices. system. 前記反撃UAVは、さらに、対抗手段発射装置を有し、該対抗手段発射装置は、前記対象航空機に向かって前記航空機対抗手段を発射し、前記対象航空機に衝突し、無力化するように作動される、請求項1に記載のシステム。 The counterattack UAV further comprises a countermeasure launcher, the countermeasure launcher being actuated to launch the aircraft countermeasure towards the target aircraft, impacting and neutralizing the target aircraft. 2. The system of claim 1, wherein 前記航空機対抗手段は、前記対抗手段発射装置により発射可能なネットを有し、前記対象航空機が捕獲され、無力化される、請求項13に記載のシステム。 14. The system of claim 13 , wherein the aircraft countermeasure comprises a net launchable by the countermeasure launcher and the target aircraft is captured and neutralized. 前記発射体発射機構は、複数の発射体を発射するように構成され、各発射体は、折り畳まれた配置で構成された反撃UAVを支持する、請求項1に記載のシステム。 2. The system of claim 1, wherein the projectile launch mechanism is configured to fire a plurality of projectiles, each projectile supporting a counterattack UAV configured in a folded configuration. 前記対象航空機は、視野を定めるセンサを有し、
前記発射体は、前記対象航空機の前記視野内にはないステルス位置から、前記反撃UAVを放出するように構成される、請求項1に記載のシステム。 the target aircraft has a sensor that defines a field of view;
2. The system of claim 1, wherein the projectile is configured to emit the counterattack UAV from a stealth location not within the field of view of the target aircraft. 対象航空機を検出し、無力化するシステムであって、
発射体発射機構と、
前記発射体発射機構から、所定の位置に発射することが可能な発射体であって、
相互にリリース可能に結合され、反撃無人航空機（UAV）を支持するように作動可能な内側チャンバを定める、少なくとも第1のハウジング区画および第2のハウジング区画から形成され、前記発射体から分離可能であり航空機対抗手段を有する、発射体と、
飛行中の対象航空機を検出するように作動可能な少なくとも一つの検出センサを有する、航空機検出システムであって、
前記対象航空機の検出の際に、前記発射機構または前記反撃UAVの少なくとも一つにコマンドデータを提供し、前記対象航空機の無力化を容易にする、航空機検出システムと、
を有し、
前記コマンドデータに基づき、前記発射体発射機構は、前記所定の位置に前記発射体を発射するように作動され、
前記コマンドデータに応じて、前記第1のハウジング区画および前記第2のハウジング区画は、相互から分離され、前記対象航空機に対する所定の位置に、前記内側チャンバから前記反撃UAVを放出し、
前記発射体からの分離の際に、前記反撃UAVは、前記航空機対抗手段により、前記対象航空機を無力化するように作動される、システム。 A system for detecting and neutralizing a target aircraft comprising:
a projectile launching mechanism;
A projectile capable of being fired at a predetermined location from the projectile launching mechanism, comprising :
formed from at least a first housing compartment and a second housing compartment releasably coupled together and defining an inner chamber operable to support a counterattack unmanned aerial vehicle (UAV), separable from said projectile; a projectile having an anti-aircraft countermeasure ;
An aircraft detection system having at least one detection sensor operable to detect a target aircraft in flight , comprising:
an aircraft detection system that, upon detection of the target aircraft, provides command data to at least one of the launch mechanism or the counterattack UAV to facilitate neutralization of the target aircraft ;
has
based on the command data, the projectile launching mechanism is activated to fire the projectile at the predetermined location;
responsive to said command data, said first housing compartment and said second housing compartment are separated from each other and eject said counterattack UAV from said inner chamber at a predetermined position relative to said target aircraft;
The system of claim 1, wherein upon separation from the projectile, the counterattack UAV is activated by the air countermeasures to neutralize the target aircraft. 前記反撃UAVは、該反撃UAVの空中輸送中、前記発射体内に折り畳まれた配置で構成され、
前記反撃UAVは、前記発射体からの分離の際に、広げられた位置に移動するように作動される、請求項17に記載のシステム。 said counterattack UAV is configured in a folded configuration within said projectile during airborne transport of said counterattack UAV;
18. The system of claim 17 , wherein the counterattack UAV is activated to move to a spread position upon separation from the projectile. 前記発射体は、前記第1および第2のハウジング区画を相互に分離するように作動されるハウジングリリース機構を有し、これにより前記対象航空機に対する所定の位置に、前記反撃UAVが放出される、請求項17に記載のシステム。 said projectile having a housing release mechanism actuated to separate said first and second housing compartments from each other thereby releasing said counterattack UAV at a predetermined position relative to said target aircraft ; 18. System according to claim 17 . 前記対象航空機に対する前記所定の位置は、前記対象航空機のセンサの視野には入らない空中位置を有する、請求項17に記載のシステム。 18. The system of claim 17 , wherein the predetermined position relative to the target aircraft comprises an aerial position that is out of view of sensors on the target aircraft. 前記コマンドデータは、妨害データ、航空機捕獲対抗手段配備コマンドデータ、対象航空機検出データ、反撃UAV制御データ、またはこれらの組み合わせの少なくとも一つを有する、請求項17に記載のシステム。 18. The system of claim 17 , wherein the command data comprises at least one of jamming data, aircraft capture countermeasure deployment command data, target aircraft detection data, counterattack UAV control data, or combinations thereof. 前記航空機検出システムは、前記反撃UAVにより支持された前記少なくとも一つの検出センサを有する、オンボード航空機検出システムを有し、
前記反撃UAVのフライト制御システムは、前記対象航空機の検出された位置に基づいて、前記反撃UAVの自動飛行を制御するように作動される、請求項17に記載のシステム。 the aircraft detection system comprises an on-board aircraft detection system comprising the at least one detection sensor carried by the counterattack UAV;
18. The system of claim 17 , wherein the counterattack UAV flight control system is operated to control automatic flight of the counterattack UAV based on the detected position of the target aircraft. 前記航空機検出システムは、前記発射体発射機構により支持された少なくとも一つの検出センサを有するオンプラットフォーム航空機検出システムを有し、
前記少なくとも一つの検出センサは、前記対象航空機を検出するように作動される、請求項17に記載のシステム。 the aircraft detection system comprises an on-platform aircraft detection system having at least one detection sensor supported by the projectile launch mechanism;
18. The system of claim 17 , wherein the at least one detection sensor is activated to detect the target aircraft. 前記航空機検出システムは、地上基地構造に関連する地上基地外部航空機検出システムを有し、
前記地上基地外部航空機検出システムは、前記少なくとも一つの検出センサを有し、
前記地上基地外部航空機検出システムは、前記発射体発射機構または前記反撃UAVの少なくとも一つに、コマンドデータを提供し、前記対象航空機の妨害および無力化が容易化されるように作動される、請求項17に記載のシステム。 the aircraft detection system comprises a ground station external aircraft detection system associated with a ground station structure;
the ground-based external aircraft detection system having the at least one detection sensor;
wherein said ground-based external aircraft detection system provides command data to at least one of said projectile launcher or said counterattack UAV and is activated such that jamming and neutralization of said target aircraft is facilitated; 18. The system of paragraph 17 . 前記反撃UAVは、飛行本体と、複数のロータ組立体とを有し、ロータ組立体の各々は、前記飛行本体の近傍に折り畳まれ、
前記複数のロータ組立体は、前記反撃UAVが前記発射体から分離された際に、前記飛行本体から広がるように構成される、請求項17に記載のシステム。 the counterattack UAV having a flight body and a plurality of rotor assemblies, each rotor assembly being folded about the flight body;
18. The system of claim 17 , wherein the plurality of rotor assemblies are configured to spread out from the flight body when the counterattack UAV is separated from the projectile . 前記プラットフォームは、少なくとも一つの移動機構を有する移動可能な移動体を有し、
前記移動可能な移動体は、地表の周囲を移動可能である、請求項17に記載のシステム。 The platform has a movable mobile body having at least one movement mechanism,
18. The system of Claim 17 , wherein the movable vehicle is movable around the surface of the earth. 前記反撃UAVは、対抗手段発射装置を有し、
前記反撃UAVは、前記対抗手段発射装置を作動させるように構成され、前記航空機対抗手段は、前記対象航空機に向かって発射され、前記対象航空機に衝突し、前記対象航空機を無力化する、請求項17に記載のシステム。 said counterattack UAV having a countermeasure launcher,
4. The counterattack UAV is configured to activate the countermeasure launcher, the aircraft countermeasure being launched toward the target aircraft, impacting the target aircraft, and neutralizing the target aircraft. 17. The system according to 17. 前記航空機対抗手段は、液体充填物を含む液体発射体を有する発射体を有し、
前記液体発射体は、前記液体充填物と組み合わされた添加剤を含む、非剛性飛行完全性部材を有し、飛行中の前記液体充填物の実質的な崩壊が抑制され、
前記液体発射体は、所定の事象の際に、流体的に分散するように構成される、請求項27に記載のシステム。 said air countermeasures having a projectile with a liquid projectile containing a liquid fill;
said liquid projectile having a non-rigid flight integrity member comprising an additive combined with said liquid fill to inhibit substantial collapse of said liquid fill during flight;
28. The system of Claim 27 , wherein the liquid projectile is configured to fluidly disperse upon a predetermined event. 前記所定の事象は、前記液体発射体を前記対象航空機に衝突させることを含み、
前記分散された液体充填物は、前記対象航空機の少なくとも一つの重大な作動装置の作動を妨害するように構成される、請求項28に記載のシステム。 the predetermined event includes impacting the liquid projectile with the target aircraft;
29. The system of claim 28 , wherein the dispersed liquid fill is configured to impede operation of at least one critical actuator of the target aircraft. 前記液体発射体は、さらに、少なくとも一つの直接衝突装置を有し、
該直接衝突装置は、前記対象航空機に衝突し、無力化するように構成され、
前記少なくとも一つの直接衝突装置は、プラスチックもしくはポリマーのペレット、金属ペレット、複合体ペレット、フィラメント素子、またはタグ形成剤を有する、請求項28に記載のシステム。 the liquid projectile further comprises at least one direct impingement device;
the direct impact device configured to impact and disable the target aircraft;
29. The system of claim 28 , wherein the at least one direct impingement device comprises plastic or polymer pellets, metal pellets, composite pellets, filament elements, or tagging agents. 対象航空機を無力化する方法であって、
飛行中の対象航空機を検出し、前記対象航空機の検出に基づいてコマンドデータを生成するステップと、
前記生成されたコマンドデータに応じて、発射体発射機構から発射体を発射するステップであって、前記発射体は、反撃無人航空機（UAV）を支持し、前記発射体は、相互にリリース可能に結合され、前記反撃UAVを収容する内側チャンバを定める、少なくとも第1のハウジング区画および第2のハウジング区画から形成される、ステップと、
前記第2のハウジング区画から前記第1のハウジング区画を分離し、前記生成されたコマンドデータに基づいて、前記対象航空機に対する所定の位置に、前記発射体の前記内側チャンバから前記反撃UAVを放射するステップと、
前記反撃UAVを作動させ、前記対象航空機を無力化するステップと、
を有する、方法。 A method of neutralizing a target aircraft comprising:
detecting a target aircraft in flight and generating command data based on the detection of the target aircraft ;
firing a projectile from a projectile launch mechanism in response to said generated command data , said projectile supporting a counterattack unmanned aerial vehicle (UAV) , said projectile being releasable relative to each other; formed from at least a first housing compartment and a second housing compartment that are joined to define an inner chamber that houses the counterattack UAV ;
separating the first housing compartment from the second housing compartment and firing the counterattack UAV from the inner chamber of the projectile at a predetermined location relative to the target aircraft based on the generated command data; a step;
activating the counterattack UAV to neutralize the target aircraft;
A method. さらに、前記発射体からの分離の際に、前記反撃UAVのロータ組立体を広げるステップを有する、請求項31に記載の方法。 32. The method of claim 31 , further comprising spreading a rotor assembly of the counterattack UAV upon separation from the projectile. さらに、前記発射体から前記反撃UAVを分離するステップは、ハウジングリリース機構を作動させるステップを有し、
前記対象航空機の検出された位置に対する所定の位置で、前記反撃UAVが放射される、請求項31に記載の方法。 further separating the counterattack UAV from the projectile comprises activating a housing release mechanism;
32. The method of claim 31 , wherein the counterattack UAV is launched at a predetermined position relative to the detected position of the target aircraft. さらに、航空機検出システムから、前記反撃UAVにコマンドデータを伝送するステップを有する、請求項31に記載の方法。 32. The method of claim 31 , further comprising transmitting command data from an aircraft detection system to the counterattack UAV. 前記対象航空機を検出するステップは、前記発射体からの分離の後、前記反撃UAVの少なくとも一つの検出センサを作動させるステップを有する、請求項31に記載の方法。 32. The method of claim 31 , wherein detecting the target aircraft comprises activating at least one detection sensor of the counterattack UAV after separation from the projectile. 前記反撃UAVを作動させ、前記対象航空機を無力化するステップは、前記反撃UAVから、前記対象航空機に向かって航空機対抗手段を発射し、前記対象航空機を無力化するステップを有する、請求項31に記載の方法。 32. The method of claim 31 , wherein activating the counterattack UAV to neutralize the target aircraft comprises firing air countermeasures from the counterattack UAV toward the target aircraft to neutralize the target aircraft. described method. 前記対象航空機を検出するステップは、前記対象航空機の動的位置を自動で追跡するステップを有する、請求項31に記載の方法。 32. The method of claim 31 , wherein detecting the target aircraft comprises automatically tracking a dynamic position of the target aircraft. さらに、前記発射体発射機構の移動機構を介して、地表に沿って、地上基地配置まで前記発射体発射機構を移動させるステップを有する、請求項31に記載の方法。 32. The method of claim 31 , further comprising moving the projectile launching mechanism along a ground surface to a ground station location via the projectile launching mechanism movement mechanism. 前記航空機を検出するステップは、さらに、前記対象航空機の既知の高度を定めるステップ、または前記対象航空機の所定の高度を予測するステップの少なくとも一つを有し、
前記所定の位置で、前記第2のハウジング区画から前記第1のハウジング区画を分離するステップは、さらに、前記第2のハウジング区画から前記第1のハウジング区画を分離し、前記コマンドデータに基づき、前記対象航空機の前記既知の高度または前記予測された高度よりも高い高度で、前記発射体の前記内側チャンバから前記反撃UAVを放出するステップを有し、これにより前記反撃UAVは、前記対象航空機のセンサにより検出されない、請求項31に記載の方法。 detecting the aircraft further comprises at least one of determining a known altitude of the target aircraft or predicting a predetermined altitude of the target aircraft;
Separating the first housing compartment from the second housing compartment at the predetermined location further comprises separating the first housing compartment from the second housing compartment and, based on the command data, ejecting the counterattack UAV from the inner chamber of the projectile at an altitude higher than the known altitude or the predicted altitude of the target aircraft, whereby the counterattack UAV is positioned above the target aircraft; 32. The method of claim 31 , undetected by a sensor. 前記反撃UAVを作動させ、前記対象航空機を無力化するステップは、前記対象航空機の作動を妨害するように構成された、航空機対抗手段を作動させるステップを有し、
前記航空機対抗手段は、可撓性絡まり素子、ネット、流体、ペレット、放電装置、または照射装置の少なくとも一つを有する、請求項31に記載の方法。 activating the counterattack UAV to neutralize the target aircraft comprises activating air countermeasures configured to impede operation of the target aircraft;
32. A method according to claim 31 , wherein the anti-aircraft means comprises at least one of flexible entanglement elements, nets, fluids, pellets, electrical discharge devices, or irradiation devices. 前記航空機検出システムは、前記対象航空機の飛行経路を追跡するように作動され、 the aircraft detection system is operated to track the flight path of the target aircraft;
前記コマンドデータに基づき、前記発射体発射機構は、前記追跡された飛行経路に基づいて、前記発射体の発射のタイミングまたは前記発射体の速度の少なくとも一つを制御するように作動される、請求項1に記載のシステム。 based on the command data, the projectile launch mechanism is actuated to control at least one of timing of firing of the projectile or velocity of the projectile based on the tracked flight path. The system of paragraph 1. 前記発射体から前記反撃UAVが放出される前記所定の位置は、前記対象航空機の既知のまたは予測された高度よりも高い高度を含む、請求項3に記載のシステム。 4. The system of claim 3, wherein the predetermined location from which the counterattack UAV is released from the projectile includes an altitude greater than a known or predicted altitude of the target aircraft. 対象航空機を無力化するシステムであって、 A system for neutralizing a target aircraft, comprising:
相互にリリース可能に結合され、反撃無人航空機（UAV）を支持するように作動された内側チャンバを定める、少なくとも第1のハウジング区画および第2のハウジング区画から形成された発射体であって、前記反撃UAVは、前記発射体から分離可能であり、航空機対抗手段を有する、発射体を有し、 A projectile formed from at least a first housing compartment and a second housing compartment releasably coupled together and defining an inner chamber actuated to support a counterattack unmanned aerial vehicle (UAV), said a counterattack UAV having a projectile separable from said projectile and having anti-aircraft means;
前記発射体または前記反撃UAVの少なくとも一つは、飛行中の対象航空機の検出の際に、航空機検出システムからのコマンドデータを受信するように作動され、 at least one of said projectile or said counterattack UAV is activated to receive command data from an aircraft detection system upon detection of a target aircraft in flight;
前記航空機検出システムは、前記対象航空機を検出するように作動された少なくとも一つの検出センサを有し、前記コマンドデータに基づき、前記発射体は、発射体発射機構により発射されるように作動され、 the aircraft detection system having at least one detection sensor actuated to detect the target aircraft, and based on the command data, the projectile being actuated to be launched by a projectile launch mechanism;
前記第1のハウジング区画および前記第2のハウジング区画は、相互に分離可能であり、前記コマンドデータに基づき、前記対象航空機に対する所定の位置で、前記内側チャンバから前記反撃UAVを放出し、 said first housing compartment and said second housing compartment being separable from each other for ejecting said counterattack UAV from said inner chamber at a predetermined position relative to said target aircraft based on said command data;
前記発射体からの前記反撃UAVの放出の際に、前記反撃UAVは、前記航空機対抗手段により前記対象航空機を無力化するように作動される、システム。 The system of claim 1, wherein upon release of said counterattack UAV from said projectile, said counterattack UAV is activated by said air countermeasures to neutralize said target aircraft. 対象航空機を無力化するシステムであって、 A system for neutralizing a target aircraft, comprising:
航空機検出システムを有し、 having an aircraft detection system,
該航空機検出システムは、 The aircraft detection system includes:
飛行中の対象航空機を検出するように作動される少なくとも一つの検出センサと、 at least one detection sensor actuated to detect a target aircraft in flight;
発射体発射機構、該発射体発射機構により発射される発射体、または前記発射体により支持され前記発射体から分離可能であり、航空機対抗手段を有する反撃無人航空機（UAV）の少なくとも一つと電子的に通信するように作動可能な、少なくとも一つの送受信器と、 electronically with at least one of a projectile launching mechanism, a projectile launched by the projectile launching mechanism, or a counterattack unmanned aerial vehicle (UAV) supported by and separable from the projectile and having air countermeasures; at least one transceiver operable to communicate with
を有し、 has
前記航空機検出システムは、前記検出に応じて、前記発射機構または前記反撃UAVの少なくとも一つにコマンドデータを提供するように作動され、前記対象航空機の無力化が容易となり、 the aircraft detection system is actuated to provide command data to at least one of the launch mechanism or the counterattack UAV in response to the detection to facilitate neutralization of the target aircraft;
前記発射体は、相互にリリース可能に結合され、前記反撃UAVを収容する内側チャンバを定める、少なくとも第1のハウジング区画および第2のハウジング区画から形成され、 said projectile is formed from at least first and second housing compartments releasably coupled to each other and defining an inner chamber containing said counterattack UAV;
前記コマンドデータに基づいて、前記発射体発射機構は、前記発射体を発射するように作動され、 based on the command data, the projectile launching mechanism is activated to fire the projectile;
前記第1のハウジング区画および前記第2のハウジング区画は、相互に分離可能であり、前記コマンドデータに応じて、前記対象航空機に対する所定の位置で、前記内側チャンバから前記反撃UAVを放出し、 said first housing compartment and said second housing compartment being separable from each other to eject said counterattack UAV from said inner chamber at a predetermined position relative to said target aircraft in response to said command data;
前記発射体からの前記反撃UAVの放出の際に、前記反撃UAVは、前記航空機対抗手段により前記対象航空機を無力化するように作動される、システム。 The system of claim 1, wherein upon release of said counterattack UAV from said projectile, said counterattack UAV is activated by said air countermeasures to neutralize said target aircraft. 対象航空機を無力化するシステムであって、 A system for neutralizing a target aircraft, comprising:
発射体発射機構と、 a projectile launching mechanism;
前記発射体発射機構により発射される発射体であって、相互にリリース可能に結合され、反撃無人航空機（UAV）を支持するように作動する内側チャンバを定める、少なくとも第1のハウジング区画および第2のハウジング区画から形成された、発射体と、 At least a first housing compartment and a second projectile fired by said projectile launching mechanism releasably coupled to each other and defining an inner chamber operative to support a counterattack unmanned aerial vehicle (UAV). a projectile formed from a housing compartment of
飛行中の対象航空機を検出するように作動される少なくとも一つの検出センサを有する航空機検出システムであって、前記検出に応じて、前記発射体発射機構、前記発射体、または前記反撃（UAV）の少なくとも一つにコマンドデータを提供するように作動され、前記対象航空機の無力化が容易化される、航空機検出システムと、 1. An aircraft detection system having at least one detection sensor actuated to detect a target aircraft in flight, wherein, in response to said detection, said projectile launch mechanism, said projectile, or said counterattack (UAV). an aircraft detection system operable to provide command data to at least one to facilitate neutralization of the target aircraft;
を有し、 has
前記コマンドデータに基づいて、前記発射体発射機構は、前記発射体を発射するように作動され、 based on the command data, the projectile launching mechanism is activated to fire the projectile;
前記第1のハウジング区画および前記第2のハウジング区画は、相互に分離可能であり、前記コマンドデータに応じて、前記対象航空機に対する所定の位置で、前記内側チャンバから前記反撃（UAV）を放出し、前記対象航空機を無力化する、システム。 Said first housing compartment and said second housing compartment are separable from each other and in response to said command data release said counterattack (UAV) from said inner chamber at a predetermined position relative to said target aircraft. , to neutralize the target aircraft.
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