| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | A method and system for managing aircraft threat data | JP51920795 | 1995-01-17 | JPH09507713A | 1997-08-05 | ジュリン，ロバート・エム; ディース，デビッド・エル |
| (57)【要約】 脅威情報のリアルタイム更新を可能にするために、使用に先立って相互視程データを計算する方法。 複数の隣接領域から構成されるエリアに対応する脅威相互視程データを計算し且つ記憶させる。 関心領域は隣接領域に中心を有する。 航空機の場所へ変化するにつれて、脅威は隣接領域から関心領域へ移動する。 ところが、脅威が初めて隣接領域の中に出現したときに相互視程データは計算されているので、そのデータを他の機能のために、それ以上の処理なしで利用することができる。 そのような他の機能は、相互視程データを脅威回避アルゴリズムに供給すること又は航空機の中で表示することを含む。 | ||||||
| 2 | Airrground bombing system | JP15821679 | 1979-12-07 | JPS5589697A | 1980-07-07 | JIYON SUTANREI AUSUMAN |
| 3 | Aerial spray method and device | JP1968187 | 1987-01-31 | JPS62223600A | 1987-10-01 | JIYOSEFU SHII FUUBAA JIYUNIA; BERAA REKUSHIYUMINARAYANA NAGA |
| 4 | METHOD AND SYSTEM FOR MANAGING AIRCRAFT THREAT DATA | EP95909265.0 | 1995-01-17 | EP0740773A1 | 1996-11-06 | DEIS, David, L.; GJULLIN, Robert, M. |
| A method for calculating intervisibility data in advance of its use for permitting a real time update of threat information. Threat intervisibility data corresponding to an area comprised of adjacent regions is calculated and stored. A region of concern is centered in the adjacent regions. As the location of an aircraft changes, threats move from an adjacent region to the region of concern. However, since the intervisibility data was calculated when the threat first appeared in the adjacent region, it is now available for other functions without further processing. Such other functions include providing it to a threat avoidance algorithms or for display within the aircraft. | ||||||
| 5 | Bomblet-Trägerkörper zum Bekämpfen von Zielobjekten mittels Bomblets | EP84105385.3 | 1984-05-12 | EP0127805A1 | 1984-12-12 | Weber, Adolf, Dipl.-Ing. |
Ein Verfahren zum Bekämpfen von Zielobjekten (27, 28) mittels Bomblets (15) und ein Bomblet-Trägerkörper (1) zum Ausüben solchen Verfahrens sollen dahingehend verbessert werden, daß die Kampfwirkung der vom Trägerkörper (1) im steilen Zielanflug achsparallel ausgestoßenen Bomblets (15) gesteigert wird. Hierfür wird oberhalb derStandard-Höhe (24) für die Belegung eines Zielgebietes (12) mit Bomblets (15) festgestellt, ob sich in einem inneren, reduzierten Zielgebiet (13) ein spezifisch zu bekämpfendes Zielobjekt (27) befindet. In diesem Falle wird der Bomblet-Ausstoß verzögert, bis der Trägerkörper (1) auf die verminderte Höhe (29), für Belegung jenes reduzierten Zielgebietes (13) mit seinen Bomblets (15), herabgefallen ist. Für die Zieldetektion im inneren Zielgebiet (13) ist in der Trägerkörper-Spitze (3) ein Sensor (4) vorausgerichtet hinter einer nach Material und Geometrie für die Sensor-Funktion optimierten Innenogive (22) angeordnet. Diese wird durch Absprengen einer flugdynamisch günstiger geformten Außenogive (19), vor Erreichen der Detektionshöhe (26) oberhalb der Standard-Höhe (24) zum Belegen des nicht-reduzierten Standard-Zielgebietes (12), freigelegt. |
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| 6 | 중복 조준 피드백을 이용한 표적 정밀 재포착 방법 | KR1020130129221 | 2013-10-29 | KR1020150049110A | 2015-05-08 | 우영권; 고은진; 이찬용; 정동길 |
| 본발명은발사무기체계의사격통제장치에서추적대상이되는표적을지정(designation)하고포착(Lock-on)하기위한중복조준피드백을이용한표적정밀재포착방법에관한것으로서, 보다상세하게는발사절차에따라사수가추적대상을중복으로조준을하며피드백할 수있게하여표적을보다정밀하게지정하고재포착할 수있도록하는중복조준피드백을이용한표적정밀재포착방법에관한것이다. 이를위해, 본발명은표적조준및 포착을위해사수에의해설정되는데이터입력값이필요한표적포착방법에있어서, 포착실패시 재조준을위해처음부터표적조준을다시수행하지않고, 기존에포착되어추적중인데이터를기준으로사격통제장치의입력값을재설정하는입력값재설정단계를수행하는것을특징으로하는중복조준피드백을이용한표적정밀재포착방법을제공한다. | ||||||
| 7 | 지능자탄 투하 시스템 | KR1020150166656 | 2015-11-26 | KR1020170061510A | 2017-06-05 | 한승조; 홍종태 |
| 본발명은, 공중에서표적정보를획득하는무인비행체; 및상기무인비행체의내부에분리가능하게장착되는적어도하나이상의지능자탄을포함하고, 상기지능자탄은,날개와상기날개를구동하는로터를구비하는지능자탄몸체; 및분리명령에의해상기지능자탄이상기무인비행체로부터분리될때, 상기지능자탄몸체로부터방출시킨상기로터를구동시켜, 표적과기설정된거리이내까지진입되도록하는구동부를포함하는것을특징으로하는지능자탄투하시스템을제공한다. | ||||||
| 8 | PHASED ARRAY LIDAR IN ORDNANCE CONTROL | US15270829 | 2016-09-20 | US20180080751A1 | 2018-03-22 | David Ginsberg; William A. Veronesi; Joseph V. Mantese; Todd Ell |
| Apparatus and associated methods relate to controlling an explosive burst event of a ballistic ordnance, based on a ground surface topography mapped by a phased-array LIDAR system. The ground surface topography is mapped using an integrated photonics LIDAR system configured to: generate a beam of coherent light; non-mechanically steer a beam of coherent light over a solid angle about an ordnance axis; and detect the beam reflected from the ground surface. The integrated photonics LIDAR system is further configured to map the ground surface topography, based on a functional relation between an angle of the beam and a time difference between generating the beam and detecting the beam reflected from the ground surface. A timing and/or direction of the explosive burst can be controlled, based on the calculated ground surface topography, so as to advantageously realize a desired effect of the explosion. | ||||||
| 9 | System and method for far-field determination of store position and attitude for separation and ballistics | US602124 | 1996-02-15 | US6069654A | 2000-05-30 | Andrew Moynihan |
| This invention relates to a system and method for far-field determination of store position and attitude for separation and ballistics. The aircraft is outfitted with two photogrammetric video cameras. The store is dropped from the aircraft and the cameras record data describing the descent of the store while the on-board avionics record data describing the flight path of the aircraft. Following the flight, the data are correlated using a computer to obtain a true store position vs. time while separating from the aircraft. | ||||||
| 10 | Spin dispensing method and apparatus | US6849 | 1987-01-27 | US4750403A | 1988-06-14 | Joseph C. Huber, Jr.; Bellur L. Nagabhushan |
| An airborne spin dispensing apparatus (100,101) and method of dispensing a plurality of sub-units (60) such that the ground plane impact pattern of the plurality of sub-units substantially corresponds to a particular geometric ground target. An onboard microprocessor (24) which receives flight data (26) and a selected target data (28) also has a program store of sub-unit ejection sequences each of which corresponds to a particular target impact geometry. The microprocessor (24) selects an appropriate sub-unit ejection sequence in accordance with the flight and selected target data and effects a release of the sub-units (60) from the spinning apparatus such that their ground impact pattern substantially matches the geometry of the ground target. | ||||||
| 11 | Exploding missile | US624042 | 1984-06-25 | US4622900A | 1986-11-18 | Wolfram Witt; Hendrick Lips; Herbert Scholler; Raimund Schweiger |
| An exploding missile has a casing and a parachute attached to the casing for making it move in a predetermined direction relative to the casing after launch. A charge in the casing has a projectile-forming front face, facing forward in the travel direction. An antenna is provided on the casing behind the front face and charge and is displaceable between a retracted position wholly behind the charge and an extended position projecting laterally therefrom and directed at least generally forwardly in the direction past the charge. An actuator is connected between the casing and the antenna for moving same from the retracted into the extended position after launch of the missile. A controller including a receiver connected to the antenna and a detonator in the charge detects the distance to a target in front of the missle and explodes the charge when a predetermined distance is detected or the target is otherwise sensed. The antenna is deployed after launch in a position capable of scanning forward of the obstacle to the secondary projectile, when that goes off. | ||||||
| 12 | Ground impact point prediction system concept for airdrops | US822753 | 1977-08-08 | US4121246A | 1978-10-17 | Delmar McLean Fadden; Alvin Richard Habbestad; James Edwin Veitengruber |
| The present invention utilizes a conventional aircraft landing and approach indicator in conjunction with a pilot controllable television camera and supporting aircraft computer for tracking an airdrop target and displaying the locus of payload ground impact points directly on the television image of the terrain being approached by the aircraft. The airdrop information is presented in such a manner which does not distract the pilot from the basic task of flying the aircraft by providing automatic calculation and continuous automatic updating of the airdrop information with respect to meteorological and aircraft flight path characteristics. | ||||||
| 13 | Method and system for computing altitude over a target and the horizontal range thereof | US27849172 | 1972-07-31 | US3921170A | 1975-11-18 | SCHMIDT DONALD J |
| Horizontal range X and altitude over a target h during bomb delivery from an aircraft at a present time t is computed by first determining horizontal range over the target Xo at time of acquisition to from the relationship
IN WHICH THE AZIMUTH ANGLE A of the target relative to the aircraft heading and the aircraft heading at a present time t is supplied by a mapping radar and a heading reference source respectively. VN and VE represent respectively the north and east components of the aircraft''s velocity supplied by a ground velocity data source. An updated estimate of the altitude, ho'', over the target at the time of target acquisition, to, is computed according to the relationship |
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| 14 | Electrical monitoring and management system for airborne ordnance | US3779129D | 1970-03-03 | US3779129A | 1973-12-18 | LAURO M |
| This disclosure relates to a system for controlling the actuation of different types of stores at various remote store stations where each store requires management in one or more operational modes prior to actuation. The type of store at each station is sensed and the store type is visually displayed at a central location. When the operator selects a store type for actuation other display means responsive to selection means and the sensing means display the operational modes of the selected store that require management prior to actuation thereof. Further display means responsive to the mode selection display to the operator the options available in each management mode. When the operator has made compatible selections in all mode options he may then actuate the selected store type.
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| 15 | Bombing instrument for targets having transverse motion relative to aircraft flight path | US3689741D | 1970-07-08 | US3689741A | 1972-09-05 | SJOBERG BENGT; VIBERG OSKAR |
| In an aircraft bombing instrument for attacks crosswind and against targets moving transversely to the line of flight, a transparent screen in the pilot''s forward field of vision displays a command symbol and an aircraft situation symbol. A switch actuation initiates a first bombing attack phase in which the display defines a sight axis that can be displaced (according to pilot selection) laterally to either side as well as downwardly relative to the aircraft''s longitudinal axis. While the pilot maneuvers the aircraft to hold the sight symbol aligned with the target, the instrument computes the aircraft velocity vector relative to the ground. A second switch actuation initiates a second phase during which display and maneuver continues as before and the instrument additionally computes the target''s position and velocity vector relative to the aircraft. A third switch actuation initiates a final phase in which displacement of the command symbol relative to the situation symbol signifies banking and pull up instructions to the pilot, in following which he flies a curving ground track. During the final phase the instrument computes the point of time and aircraft velocity vector at which a bomb must be released to hit the target and the bank and pull up required to achieve these, controls the command display accordingly, and issues a release impulse at the proper time.
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| 16 | Altimeter ranging | US59803256 | 1956-07-16 | US2988816A | 1961-06-20 | HELGESON VIRGIL L; LOPER EDWARD J |
| 17 | Object detecting and locating system | US44357342 | 1942-05-19 | US2952014A | 1960-09-06 | CALDWELL JR JOSEPH J |
| 18 | Bombing control | US54350544 | 1944-07-04 | US2767616A | 1956-10-23 | STEIN JAMES H |
| 19 | Radio scanning apparatus | US64221646 | 1946-01-19 | US2720643A | 1955-10-11 | HAYS JR ROBERT F |
| 20 | Radio bomb release system with warning period | US59018445 | 1945-04-25 | US2441657A | 1948-05-18 | DANIEL BLITZ |
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