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51. 发明公开

EP0148704A3 Monitoring method for target localization by way of an unmanned aircraft 有权转让
标题翻译：通过未经规定的飞机的方式进行目标定位的监测方法
公开(公告)号：EP0148704A3
公开(公告)日：1985-08-28
申请号：EP84402736
申请日：1984-12-27
申请人： THOMSON-CSF
发明人： Losfelt, Denis
IPC分类号： G01C21/22 , F41G07/22 , G01S05/00
CPC分类号： G01C21/22 , F41G7/2206 , F41G7/2253 , F41G7/2293 , F41G7/30 , G05D1/0038 , G05D1/0044

52. 发明公开

EP3255371A1 AIRCRAFT CONTROL DEVICE, AIRCRAFT, AND METHOD FOR COMPUTING AIRCRAFT TRAJECTORY 有权
标题翻译：飞机控制装置，飞机和用于计算飞机轨道的方法
公开(公告)号：EP3255371A1
公开(公告)日：2017-12-13
申请号：EP16827646.7
申请日：2016-07-11
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： YAMASAKI, Koichi
IPC分类号： F41H13/00 , B64C19/02 , G08G5/00
CPC分类号： G05D1/12 , B64C19/02 , F41G7/24 , F41G7/30 , F41G9/002 , F41H13/00 , G05D1/0005 , G05D1/0094 , G05D1/104 , G05D1/107
摘要： In the present invention, an aircraft control device computes the trajectories of a plurality of formation-flying aircraft using a calculation method; e.g., direct collocation with nonlinear programming (DCNLP), in which the optimal solution is obtained by discretizing continuous variables. Trajectory-indicating nodes are computed and set by plugging discretized aircraft control variables into an aircraft motion equation or by using another method. Using discretization to address aircraft trajectories reduces complexity and allows the trajectories to computed more rapidly than with computations involving chronologically contiguous aircraft trajectories. The aircraft control device determines the optimal trajectory, among trajectories that comply with constraints corresponding to the role of the aircraft, on the basis of an assessment value obtained by an objective function corresponding with the role. Accordingly, the aircraft control device is capable of performing computations more rapidly on more suitable trajectories corresponding with the role of the aircraft.
摘要翻译：在本发明中，飞行器控制装置使用计算方法来计算多个编队飞行器的轨迹，例如直接与非线性规划搭配（DCNLP），其中最优解通过离散化连续变量而获得。轨迹指示节点通过将离散化的飞行器控制变量插入飞机运动方程或通过使用另一种方法来计算和设置。使用离散化来解决飞机轨迹降低了复杂性，并且允许轨迹的计算比涉及按时间顺序连续的飞机轨迹的计算更快。飞行器控制装置基于由与该角色相对应的目标函数获得的评估值来确定符合与飞机的角色相对应的约束的轨迹之中的最优轨迹。因此，飞机控制装置能够更加快速地在与飞机的作用对应的更合适的轨迹上执行计算。

53. 发明授权

EP2802838B1 ANTI-ROCKET SYSTEM 有权
标题翻译： RAKETENABWEHRSYSTEM
公开(公告)号：EP2802838B1
公开(公告)日：2017-03-29
申请号：EP13704497.0
申请日：2013-01-10
申请人： Israel Aerospace Industries Ltd.
发明人： ROVINSKY, Jacob
IPC分类号： F41G7/30 , F41H11/02 , G01S7/00 , G01S13/00 , G01S13/87 , F42B15/01
CPC分类号： F41H11/02 , F41G7/30 , F41G7/303 , F42B15/01 , G01S7/003 , G01S13/003 , G01S13/878

54. 发明公开

EP3118563A1 VERFAHREN ZUM SCHÜTZEN EINES FAHRZEUGS VOR EINEM ANGRIFF DURCH EINEN LASERSTRAHL 有权转让
标题翻译：方法用于保护车辆前面有攻击由激光束
公开(公告)号：EP3118563A1
公开(公告)日：2017-01-18
申请号：EP16001535.0
申请日：2016-07-12
申请人： Diehl BGT Defence GmbH & Co. KG
发明人： Nolte, Arne , Masur, Michael , Groß, Michael , Künzner, Nicolai , Kuhn, Thomas , Stelte, Norbert
IPC分类号： F41H11/00 , F41H13/00 , F42B15/01 , F41G7/26
CPC分类号： F41H11/00 , F41G7/2253 , F41G7/2293 , F41G7/30 , F41H13/00 , F42B15/01
摘要： Die Erfindung geht aus von einem Verfahren zum Schützen eines Fahrzeugs (2) vor einem Angriff durch einen Laserstrahl (8).
Das Fahrzeug (2) kann schnell und damit wirkungsvoll gegen einen Hochenergielaserstrahl (8) geschützt werden, wenn ein Sensorsystem (16) des Fahrzeugs (2) Laserstrahlung des Laserstrahls (8) detektiert und eine Steuereinheit (20) des Fahrzeugs (2) den Laserstrahl (8) aus den Daten des Sensorsystems (16) als solchen erkennt, ein Start eines Lenkflugkörpers (12, 14) zum Schutz des Fahrzeugs (2) vor dem Laserstrahl (8) von der Steuereinheit (20) gesteuert wird und der Lenkflugkörper (12, 14) vom Fahrzeug (2) aus startet.
摘要翻译：本发明涉及一种用于通过激光束（8）的保护的车辆（2）免受攻击的方法。车辆（2）可以快速和有效地与一个高能量的激光束被保护（8）中，当一个传感器的车辆（2）的系统（16）检测的激光束（8）的车辆（2）的激光束的激光辐射以及控制单元（20）（8）从所述传感器系统的数据（16）识别为这样，一个导弹（12，14）的开始为在从所述控制单元（20）被控制和导弹的激光束（8）的前面保护车辆（2）（12 ，14）在车辆的（2）从开始。

55. 发明公开

EP2678708A1 ELECTRONIC SYSTEM FOR THE IDENTIFICATION AND NEUTRALIZATION OF MENACES IN A PREDEFINED AREA 审中-公开
标题翻译： EELEKTRONISCHES系统的识别和中和威胁的预定区域中
公开(公告)号：EP2678708A1
公开(公告)日：2014-01-01
申请号：EP11713041.9
申请日：2011-02-21
申请人： Oto Melara S.p.A.
发明人： IARDELLA, Carlo, Alberto
IPC分类号： G01S13/00 , G01S13/87 , F41G5/08 , F41G7/30 , F41H13/00
CPC分类号： F41G7/30 , F41G3/14 , F41G5/08 , F41H11/02 , G01S13/003 , G01S13/87
摘要： An electronic system for the identification and the neutralization of menaces in a predefined area through radar detection comprising at least three discovery radars (R1,R2,R3) arranged on the vertices of a triangle at a predefined distance among them, within said area to be protected and a processing electronic unit (CPU) for receiving from each of said discovery radars information related to the ballistic menace, for recognizing the ones deriving from the same menace, for each of them, through a triangulation algorithm, for identifying three-dimensional position and speed.

56. 发明公开

EP2443412A1 SYSTEM, APPARATUS AND METHOD FOR PROTECTION OF A VEHICLE AGAINST A POSSIBLE THREAT 审中-公开
标题翻译：系统，设备及方法车辆在潜在危险保护
公开(公告)号：EP2443412A1
公开(公告)日：2012-04-25
申请号：EP09846262.5
申请日：2009-06-16
申请人： Saab AB
发明人： ZÄTTERQVIST, Christer
IPC分类号： F41H11/02 , F42B12/36 , F42B12/46 , F42B12/56
CPC分类号： F41H11/02 , F41G7/30 , F42B12/46 , F42B12/56
摘要： The invention relates to a system for protection of a vehicle (2) against a possible threat (4) approaching the vehicle. The system comprises a sensor (6) that detects the possible threat, a control unit (8) that evaluate the possible treat and transmit processed information, a counter-measure apparatus (2), and a launcher (10) that receives a launching signal from the control unit for launching the counter-measure apparatus towards (D1) the threat when the treat is confirmed. The counter-measure apparatus (2) comprises a guiding unit (12) by which the counter-measure apparatus (2) is guided towards the threat (4) based on the processed information of the threat that is continuously received via the control unit (8), during acceleration of the counter-measure apparatus (2). The counter-measure apparatus further comprises a counter-measure element (14,18) that is launched in a direction (D2) against the threat (4) by means (16) for releasing and activating the counter-measure element (14,18), when the counter- measure apparatus (2) has reached within the vicinity of the threat (4), such that the counter-measure element (14,18) can defeat the threat (4). The invention also relates to an apparatus and a method for protection of a vehicle against a possible threat approaching the vehicle.

57. 发明公开

EP1626245A1 Guided missile with distributed guidance mechanism 审中-公开
标题翻译： Lenkflugkörpermit verteiltem Lenkungsmechanismus
公开(公告)号：EP1626245A1
公开(公告)日：2006-02-15
申请号：EP05254970.6
申请日：2005-08-10
申请人： Rafael Armament Development Authority Ltd.
发明人： Fein,Assa , Ben-Horin, Ronen
IPC分类号： F41G7/22
CPC分类号： F41G7/2206 , F41G7/2233 , F41G7/30 , F41G7/308
摘要： A weapons system (20) including a guided missile (22) and a guidance mechanism, separate from the guided missile. The guided missile includes a seeker (12) for producing signals indicative of a position of a target, and a steering mechanism (18) for steering the guided missile. The guidance mechanism controls the steering mechanism (18) based on the signals, so as to steer the guided missile (22) towards the target.
摘要翻译：与导弹分离的包括导弹（22）和引导机构的武器系统（20）。导弹包括用于产生指示目标位置的信号的探测器（12）和用于转向导弹的转向机构（18）。引导机构基于信号控制转向机构（18），以便将导弹（22）转向目标。

58. 发明授权

EP0887613B1 Procédé de programmation en vol d'un instant de déclenchement d'un élément de projectile, conduite de tir et fusée mettant en oeuvre un tel procédé 失效
标题翻译：在飞行中用于触发地板元件，消防时刻和雷管用于实施该方法编程方法
公开(公告)号：EP0887613B1
公开(公告)日：2003-08-20
申请号：EP98104650.1
申请日：1998-03-14
申请人： GIAT INDUSTRIES
发明人： Lamorlette, Gérard , Bredy, Thierry
IPC分类号： F41G7/30
CPC分类号： F41G7/30 , F42C11/065 , F42C17/04 , G01P3/665

59. 发明授权

EP0222570B1 Missile guidance systems 失效
标题翻译：指导系统错误
公开(公告)号：EP0222570B1
公开(公告)日：1993-06-30
申请号：EP86308529.6
申请日：1986-10-31
申请人： BRITISH AEROSPACE PUBLIC LIMITED COMPANY
发明人： Salkeld, David British Aerospace PLC
IPC分类号： F41G7/30
CPC分类号： F41G7/30

60. 发明公开

EP0064168A1 Jitter compensated scene stabilized missile guidance system 失效
标题翻译：装置用于补偿在稳定的导弹制导系统中的抖动。
公开(公告)号：EP0064168A1
公开(公告)日：1982-11-10
申请号：EP82102966.7
申请日：1982-04-07
申请人： Hughes Aircraft Company
发明人： Zwirn, Robert , Bozeman, John W.
IPC分类号： F41G7/30
CPC分类号： F41G7/30
摘要： An improved missile guidance system is provided which automatically compensates for jitter motion of the optical sight of a video tracker. The invention is adapted to receive video data input from an infrared detector or conventional camera (12). The invention includes circuits for filtering, gating, and digitalizing the incoming data as well as a formatter for directing successive frames into memory. Two memories (36, 40) are provided; the contents of which are sampled by matching logic (42) as the second memory is being loaded. The matching logic (42) thereby compares one frame of data to another at plurality of positions and provides a signal to an address latch (46) when the best match is obtained. The format circuitry (32) provides the position information to the address latch where it is stored for further processing. The output of the address latch is filtered to eliminate any signals representative of intentional tracking motion. The filtered output thus provides the jitter correction to the missile guidance system (60) where missile guidance signals are compensated by the jitter correction.

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