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1. 发明申请

US20190249956A1 METHOD FOR DETERMINING CHARACTERISTIC-CURVE CORRECTION FACTORS OF A MATRIX DETECTOR THAT IMAGES IN THE INFRARED SPECTRAL RANGE, METHOD FOR CONTROLLING A GUIDED MISSLE AND GUIDED MISSLE 审中-公开
公开(公告)号：US20190249956A1
公开(公告)日：2019-08-15
申请号：US16270637
申请日：2019-02-08
申请人： DIEHL DEFENCE GMBH & CO. KG
发明人： FLORIAN GAGEL
IPC分类号： F41G7/22 , H04N5/33
CPC分类号： F41G7/007 , F41G7/001 , F41G7/2293 , G01S3/7803 , H04N5/33 , H04N5/357 , H04N17/002
摘要： The invention relates to a method for determining characteristic-curve correction factors a matrix detector that images in the infrared spectral range. A good image correction can be obtained by virtue of an area of homogeneous temperature being recorded at two different temperatures by the matrix detector, there being two images with different integration times for each temperature. A signal gradient over the integration time is established for each of the pixels from the four pixel values at the two temperatures in each case and the gain being established from the difference of the signal gradients and characteristic-curve correction factors for the gain being stored.

2. 发明授权

US09897417B2 Payload delivery 有权
公开(公告)号：US09897417B2
公开(公告)日：2018-02-20
申请号：US15100453
申请日：2014-12-04
申请人： BAE SYSTEMS PLC
发明人： Andrew Christopher Tebay
IPC分类号： G05D1/00 , F41G3/22 , F41G7/00 , F41G9/00 , G05D1/10 , B64C39/02 , G06Q50/32 , G06Q10/00 , G06Q10/04 , B64D1/02 , F41G3/08 , G05D1/12 , G06K9/00 , G08G5/00 , H04N5/232 , G06T7/73
CPC分类号： F41G3/22 , B64C39/024 , B64C2201/127 , B64C2201/128 , B64C2201/141 , B64C2201/146 , B64D1/02 , F41G3/08 , F41G7/007 , F41G9/002 , G05D1/0094 , G05D1/101 , G05D1/12 , G06K9/0063 , G06Q10/00 , G06Q10/04 , G06Q50/32 , G06T7/73 , G08G5/0034 , H04N5/232
摘要： Disclosed is a method for delivering a load on-board an aircraft to a target. The method comprises: acquiring a position of the target; acquiring parameter values relating to aircraft maneuverability; acquiring load properties; acquiring parameter values relating to environmental conditions; using the acquired information, determining a position and a velocity value; performing, by the aircraft, the procedure; and, at a point in the procedure that the aircraft has the determined position and its travelling at a velocity equal to the determined velocity value, releasing the load. The determined position and velocity value are such that, were the aircraft to release the load while having the determined position and velocity, the load would travel to be within a predetermined distance of the target. The procedure is such that the aircraft would have the determined position and velocity at some time-step.

3. 发明授权

US09803958B2 Weapons stores processor panel for aircraft 有权
公开(公告)号：US09803958B2
公开(公告)日：2017-10-31
申请号：US13401993
申请日：2012-02-22
申请人： Justin L. Wolfanger , Carlo Asaro
发明人： Justin L. Wolfanger , Carlo Asaro
IPC分类号： F41G3/22 , B64D7/00 , B64C27/04 , F41A19/58 , F41G7/00
CPC分类号： F41G3/22 , B64C27/04 , B64D7/00 , F41A19/58 , F41G7/007
摘要： An aircraft weapons control system including a weapons stores processor panel for receiving input signals from a weapons input; a weapons interface for receiving fire signals from the weapons stores processor panel to control firing of aircraft weapons; and a flight management system in communication with the weapons stores processor panel and the weapons interface, the flight management system providing control signals to the weapons interface; wherein the weapons stores processor panel implements safety interlocks to prevent or enable firing of the aircraft weapons.

4. 发明申请

US20160298932A1 SYSTEM AND METHOD FOR DECOY MANAGEMENT 审中-公开
标题翻译：系统和方法进行管理
公开(公告)号：US20160298932A1
公开(公告)日：2016-10-13
申请号：US15158028
申请日：2016-05-18
申请人： The Government of the United States of America, as represented by the Secretary of the Navy
发明人： Timothy P. McGeehan
IPC分类号： F41G7/22 , F41J9/08 , F41G7/00
CPC分类号： F41G7/224 , F41G7/007 , F41J9/08
摘要： System and method for determining which decoys should not be deployed based on the locations of the nearby high value units and other considerations. The system and method can visualize and manage the employment of decoys in a multi-platform environment by plotting the predicted path of decoys relative to high value unit (HVU) motion, and highlighting any situations that exist where the decoys (both air-drifting and self-propelled) launched from a platform can direct an incoming threat towards a high value unit. The system and method can develop, display, and automatically transmit a recommendation to launch or not launch a specific decoy.
摘要翻译：根据附近高价值单位的位置和其他考虑，确定不应部署哪些诱饵的系统和方法。该系统和方法可以通过绘制相对于高值单位（HVU）运动的预测诱饵路径，在多平台环境中可视化和管理诱饵的使用，并突出显示任何存在于诱饵（空气漂移和自推进）可以将进入的威胁引导到高价值单位。该系统和方法可以开发，显示和自动传送推出或不启动特定诱饵的建议。

5. 发明授权

US09453708B2 Method for determining position data of a target object in a reference system 有权
标题翻译：用于确定参考系中目标对象的位置数据的方法
公开(公告)号：US09453708B2
公开(公告)日：2016-09-27
申请号：US13091664
申请日：2011-04-21
申请人： Michael Holicki , Nikolaus Schweyer , Johannes Speth , Juergen Zoz
发明人： Michael Holicki , Nikolaus Schweyer , Johannes Speth , Juergen Zoz
IPC分类号： G06K9/00 , F41G7/22 , G01S3/786 , G06K9/32
CPC分类号： F41G7/2226 , F41G3/02 , F41G7/007 , F41G7/2246 , F41G7/2253 , F41G7/2293 , G01S3/7865 , G06K9/3241
摘要： A method for determining the position data of a target object in a reference system from an observation position at a distance. A three-dimensional reference model of the surroundings of the target object is provided, the reference model including known geographical location data. An image of the target object and its surroundings, resulting from the observation position for an observer, is matched with the reference model. The position data of the sighted target object in the reference model is determined as relative position data with respect to known location data of the reference model.
摘要翻译：一种用于从距离的观察位置确定参考系中的目标对象的位置数据的方法。提供目标对象周围的三维参考模型，该参考模型包括已知的地理位置数据。由观察者的观察位置产生的目标对象及其周围的图像与参考模型相匹配。将参考模型中的目标对象的位置数据确定为相对于参考模型的已知位置数据的相对位置数据。

6. 发明申请

US20160195878A1 MISSILE SYSTEM WITH NAVIGATION CAPABILITY BASED ON IMAGE PROCESSING 审中-公开
标题翻译：基于图像处理的导航能力的MISSILE系统
公开(公告)号：US20160195878A1
公开(公告)日：2016-07-07
申请号：US14911469
申请日：2014-06-15
申请人： RAFAEL ADVANCED DEFENSE SYSTEMS LTD
发明人： Omri PELEG , Eran SHIMONOVITZ , Avfram LEVY
IPC分类号： G05D1/10 , F41G7/34 , G05D1/00 , F42B15/01 , F41G7/22
CPC分类号： G05D1/107 , F41G7/007 , F41G7/008 , F41G7/2206 , F41G7/2213 , F41G7/2253 , F41G7/2293 , F41G7/30 , F41G7/343 , F42B15/01 , G01C21/12 , G01S5/16 , G05D1/0038
摘要： The present invention relates to electro-optic guided missile systems and, in particular, it concerns systems and methods providing enhanced navigation capabilities based on ego-motion processing of seeker images. The missile system comprising: a missile; a seeker located at a nose portion of said missile, said seeker comprising an electro-optic imaging sensor; and a control arrangement for steering the missile along a flight path to a target, characterized in that the missile system further comprises: a navigation subsystem receiving images from said imaging sensor, said navigation subsystem being configured to: co-process a plurality of said images from said imaging sensor to derive ego-motion of said missile relative to a region viewed by said imaging sensor; derive from said ego-motion a calculated target direction from said missile to a target.
摘要翻译：本发明涉及电光导弹系统，特别涉及提供基于探测器图像的自动运动处理的增强导航能力的系统和方法。导弹系统包括：导弹; 位于所述导弹的鼻部的探测器，所述探测器包括电光成像传感器; 以及用于将导弹沿着飞行路径转向目标的控制装置，其特征在于，所述导弹系统还包括：导航子系统，从所述成像传感器接收图像，所述导航子系统被配置为：协同处理多个所述图像从所述成像传感器导出所述导弹相对于由所述成像传感器观看的区域的自身运动; 从所述自我运动导出从所述导弹到目标的计算目标方向。

7. 发明授权

US08927915B1 Detection of rocket body through an active firing plume 有权
标题翻译：通过主动发射羽流来检测火箭体
公开(公告)号：US08927915B1
公开(公告)日：2015-01-06
申请号：US13531286
申请日：2012-06-22
申请人： Frank O. Clark
发明人： Frank O. Clark
IPC分类号： F41G7/22 , F42B15/01 , F41G7/00 , F42B15/00
CPC分类号： F41H11/02 , F41G3/14 , F41G7/007
摘要： Apparatus and a method for intercepting a rocket body during boost phase. A sensor is arranged to detect thermal emission in a range that is characteristic of a firing rocket body. The image detected by the sensor is applied to an analog-to-digital converter for digitization and application to a computer that includes a routine for separating the modulated photon energy of the detected image from the substantially unmodulated photon energy that characterizes rocket body emissions. The unmodulated photon energy, signature of the rocket body, may be utilized by a fire control system for tracking, targeting and aiming munitions at the firing rocket body.
摘要翻译：在升压阶段拦截火箭体的装置和方法。传感器被布置成在发射火箭体的特征的范围内检测热发射。由传感器检测到的图像被应用于模拟数字转换器，用于数字化并应用到包括用于将检测到的图像的调制光子能量与表征火箭体发射的基本上未调制的光子能量分离的例程的计算机。消防系统可以使用未调制的光子能量，即火箭体的签名，用于跟踪，瞄准和瞄准射击火箭弹体上的弹药。

8. 发明授权

US08686879B2 Graphical display for munition release envelope 有权
标题翻译：用于弹药释放包络的图形显示
公开(公告)号：US08686879B2
公开(公告)日：2014-04-01
申请号：US13119790
申请日：2008-09-25
申请人： Richard H. Lammers , Greg Boria
发明人： Richard H. Lammers , Greg Boria
IPC分类号： G01C21/00
CPC分类号： F41G9/002 , F41G7/007 , G01C23/00
摘要： A method and module for displaying a munition release envelope.
摘要翻译：用于显示弹药释放信封的方法和模块。

9. 发明授权

US08674276B2 Defense system 有权
标题翻译：防御体系
公开(公告)号：US08674276B2
公开(公告)日：2014-03-18
申请号：US13052498
申请日：2011-03-21
申请人： Jacob Rovinsky
发明人： Jacob Rovinsky
IPC分类号： F42B15/01 , F41G7/20 , F42B15/00 , F41G7/00
CPC分类号： F41H11/02 , F41G7/007 , F41G7/2206 , F41G7/224 , F42B12/22 , F42B12/58 , F42B15/10
摘要： An exo-atmospheric intercepting method for intercepting in space multiple objects, including acquiring and tracking multiple inflated objects which fly towards a protected territory. The method further includes launching an interceptor missile accommodating a plurality of kill vehicles each hosting a plurality of punching objects and classifying the multiple objects into clusters. In respect of each cluster of objects, determining an ejection condition responsive to meeting of which a kill vehicle is ejected from the interceptor missile towards the cluster of objects and thereafter releasing from the kill vehicle a plurality of punching objects such that every inflated object in the cluster is likely, with a high degree of certainty, to be punched by one or more punching objects.
摘要翻译：一种用于在空间中拦截多个物体的外部大气截获方法，包括获取和跟踪飞向受保护地区的多个膨胀物体。该方法还包括发射拦截器导弹，其容纳多个杀死车辆，每个主机都承载多个冲孔物体并将多个物体分类成群集。对于每个物体群，确定一个弹出条件，该弹出状态响应于一个杀伤车辆从拦截弹导弹朝向物体群集弹出，然后从杀死的车辆上释放出多个穿孔物体，集群很可能以高度的确定性被一个或多个冲孔物体冲压。

10. 发明授权

US08544375B2 System and method for providing a cooperative network for applying countermeasures to airborne threats 有权
标题翻译：提供合作网络的系统和方法，将对策应用于机载威胁
公开(公告)号：US08544375B2
公开(公告)日：2013-10-01
申请号：US10590830
申请日：2004-12-23
申请人： Arnold Kravitz
发明人： Arnold Kravitz
IPC分类号： F41H11/02
CPC分类号： F41G7/224 , F41G7/007 , F41H11/02
摘要： A system and method capable of providing a cooperative network for applying countermeasures to airborne threats is provided. The system contains at least one aircraft having an airborne countermeasures system (ACS) capable of controlling deployment of countermeasures located on the aircraft. The system also contains a central countermeasures management system (CCMS) capable of communicating with the ACS to control the ACS in deployment of the countermeasures located on the aircraft. The aircraft may be one of a series of aircrafts, where each aircraft within the series of aircrafts has a separate ACS thereon, and where each separate ACS is capable of controlling deployment of countermeasures located on an aircraft within the series of aircrafts on which the separate ACS is located. When multiple aircrafts are within the network, the CCMS is capable of communicating with each separate ACS in response to the airborne threat, to control deployment of the countermeasures.
摘要翻译：提供了一种能够提供用于将对策应用于机载威胁的协作网络的系统和方法。该系统至少包含一架具有能够控制飞机上对抗部署的机载对抗系统（ACS）的飞机。该系统还包含一个中央对策管理系统（CCMS），能够与ACS进行通信，以控制ACS部署飞机上的对策。飞机可以是一系列飞机之一，其中一系列飞机内的每架飞机在其上具有单独的ACS，并且其中每个单独的ACS能够控制位于该系列飞机内的飞机上的对策的部署，其上分开 ACS位于。当多个飞机在网络内时，CCMS能够响应于机载威胁与每个单独的ACS进行通信，以控制对策的部署。

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