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公开(公告)号：WO2022066131A1
公开(公告)日：2022-03-31
申请号：PCT/TR2021/050976
申请日：2021-09-24
摘要： Invention relates to an optimal weapon routing system providing cause of maximum destruction to targets within effect radius (r) by one single shot and comprises at least a sensor (2) detecting and transmitting coordinates, importance level, sizes and/or shapes of targets, a control unit (1) detecting the instant coordinates (xG, yG) of the optimal point that will cause maximum destruction to the targets in line with the data transmitted by sensors (2) instantly, and conducting instant route updating, adjusting the push power of weapon engine and the angles of flaps according to the route data, a power unit (4) providing movement of weapon at the adjusted speed in the route direction specified by control unit (1), an energy unit (5) providing the energy required for running the power unit (4) and at least an explosive (3) exploding upon arrival of the weapon to the optimal route coordinates, providing destruction of all targets within range of effect radius (r).
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公开(公告)号：WO2021167662A1
公开(公告)日：2021-08-26
申请号：PCT/US2020/060845
申请日：2020-11-17
申请人： RAYTHEON COMPANY
摘要： Imaging and ALPD device and method of use is disclosed. A detector (104) generates an electrical signal in response to receiving an optical signal (115), wherein a frequency of the electrical signal is indicative of a frequency of the optical signal. A first detection/readout circuit (ROIC1) is sensitive to a first frequency range, and a second detection/readout circuit (ROIC2) is sensitive to a second frequency range. The first detection/readout circuit allows the electrical signal to pass from the first detection/readout circuit to the second detection/readout circuit.
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公开(公告)号：WO2019016671A1
公开(公告)日：2019-01-24
申请号：PCT/IB2018/055242
申请日：2018-07-16
发明人： M., Jeyakumar , KUMAR, Narendra , PRASAD, Kamlesh , SINGH, Satya Pal , GUPTA, Atul , SINGH, Abhay Kumar , SHUKLA, Rahul , N., Ramachandran , R., Kathiravan , K., Amirtha Ganesh , J., Jeyandran , L., Jayanthi , R., Rakesh , I., Karthic Subramaniyan , J., Kesavan , C., Narmadha , C., Ramachandradurai , L., Sarojini , V., Hamsadhwani
摘要： The present disclosure envisages a computer-implemented elector-pneumatic projectile launching training system (1000) for real-time simulation, which is easily reconfigurable for a variety of indoor and outdoor applications. The training system (1000) is configured for training at least one trainee by at least one instructor which can also be expanded to train three sets of trainees and instructors. The training system (1000) comprises of a computer- implemented simulation system employing electro-optical sensors (230) networked in wired and wireless means. This system employs scaled model of target mounted on an automated battery operated vehicle (260) and/or remotely controlled or real aerial simulated target system, a simulated projectile and a target, an electro-mechanically actuated motion simulator projectile launching mechanism (100), means for locking of the projectile inside the launching mechanism, a control unit, a trigger, a sensor, a repository 250 and a performance monitoring module (310). The trigger releases the pneumatic lock thereby letting the hydraulically compressed spring, launching the dummy projectile. The control unit (200) in combination with the performance monitoring and report generator module (310) is the nerve centre of the entire training system (1000), which is operable by one or more instructor(s) to generate any type of simulation or audio visual indications including emergencies associated with the simulated launching of projectile at the said target system (260) and store the results in the repository post processing by the performance monitoring and report generator (310). The array of networked optical tracking sensors (230) capture an image/video of the target and transmit it over the wireless trans-receiver (240) module to the display unit (220) of the said control unit (200) which in turn transfers it to the performance monitoring and report generator (310) for analysis and report generation. The repository 250 stores the image and the video. The crossover range trans-receiver (280) transmits the positional data of the target including the programmable aerial target (270), to the digital control unit (200) which is combined with the inputs of standalone and integrated optical tracking module (230) received via voice a wireless trans-receiver module (240). The Portable Indoor Training System (300) comprises of the Performance Monitoring and Report Generator Module (310) which is common to all the indoor and outdoor configurations, visor mounted display module (320) which can also be used in combination with motion simulator (100). The indoor display and audio visual components (330) and comparator and computing module (340) combine to impart indoor training based on the preloaded target parameters and the trainee's action with the specially configured launching tube and launching mechanism. The multisource power supply unit (400) comprises of conventional and renewable energy sources wherein this module also comprises of phase convertor equipment also to cater for the need of 3-phase power supply for components of motion simulator (100). The voice communication module (600) is integrated with the digital control unit (200) to enable one- way point-to-point communication from instructor trainee. The Observer and Instructor Training Kit (700) are also part of the training system (1000) wherein the digital control unit and performance monitoring and report generator module (310) are used in conjunction with all types of target systems.
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公开(公告)号：WO2018226266A1
公开(公告)日：2018-12-13
申请号：PCT/US2018/017897
申请日：2018-02-13
申请人： RAYTHEON COMPANY
摘要： A thermal detection system for detecting a thermal profile of an optical window may be used in an airborne body that contains a sensor system. The system may include a thermal imager arranged within the airborne body for imaging a portion of the optical window and the portion may coincide with an optical path of the sensor system. The system may further include a processor in communication with the thermal imager for receiving images of the portion and determining a thermal gradient of the portion. The processor may be configured to apply corrections to active optical elements of the sensor system to accommodate for adverse thermal effects on the optical sensor that interferes with the sensor system performance.
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公开(公告)号：WO2017048348A1
公开(公告)日：2017-03-23
申请号：PCT/US2016/041158
申请日：2016-07-06
申请人： RAYTHEON COMPANY
CPC分类号： G01S3/786 , F41G7/008 , F41G7/2213 , F41G7/2246 , F41G7/2253 , F41G7/2293 , G01C3/08 , G01S7/4813 , G01S7/4818 , G01S17/66 , G02B6/0005 , G02B17/008
摘要： A dual-mode active and passive gimbaled optical system including a mechanism for coupling an optical signal from an off-gimbal active-mode source into the on-gimbal passive-mode optical path. One example of the system includes a passive off-gimbal detector assembly configured to image emissive electromagnetic radiation from a viewed scene, and a receiver-path optical assembly, including on-gimbal objective optics, that directs the electromagnetic radiation to the off-gimbal detector assembly. The system further includes an off-gimbal active source that generates an optical signal, a gimbal bearing assembly that supports rotation of the gimbal and includes a centrally-located output ferrule mated to an optical fiber that transports the optical signal from the active source to the output ferrule, and an on-gimbal optical coupling element that receives the optical signal from the output ferrule and couples the optical signal into the receiver optical path to direct the optical signal toward the on-gimbal objective optics.
摘要翻译： 一种双模有源和无源万向平衡光学系统，包括用于将光信号从非万用主动模式源耦合到万用无源模式光路中的机构。 该系统的一个示例包括被配置成对来自观看场景的发射电磁辐射进行成像的无源非万用节点检测器组件，以及包括物镜光学元件的接收器路径光学组件，其将电磁辐射引导到非万用节点检测器 部件。 该系统还包括产生光学信号的万向节活动源，支撑万向节的旋转的万向轴承组件，并且包括与光纤配合的居中定位的输出套圈，所述光纤将光信号从活动源传送到 输出套圈以及从所述输出套圈接收所述光信号并将所述光信号耦合到所述接收器光路中以将所述光信号引导到所述物镜光学元件的万向光耦合元件。
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公开(公告)号：WO2017019154A1
公开(公告)日：2017-02-02
申请号：PCT/US2016/033032
申请日：2016-05-18
申请人： RAYTHEON COMPANY
摘要： A dual-mode optical and RF reflector, and test system using the same. In one example the reflector is a mirror having a reflective surface including a first zone having a first surface precision, wherein a remainder of the reflective surface outside of the first zone has a second surface precision that is substantially lower than the first surface precision, the mirror being configured to collimate and reflect an RF signal from the reflective surface, and to collimate and reflect an optical signal from the first zone.
摘要翻译： 双模光学和RF反射器，以及使用其的测试系统。 在一个示例中，反射器是具有反射表面的反射镜，反射表面包括具有第一表面精度的第一区域，其中第一区域外部的反射表面的其余部分具有基本上低于第一表面精度的第二表面精度， 镜被配置成从反射表面准直和反射RF信号，并准直并反射来自第一区的光信号。
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公开(公告)号：WO2015001556A1
公开(公告)日：2015-01-08
申请号：PCT/IL2014/050590
申请日：2014-07-01
发明人： LEVY, Benjamin , GOLDBERG, Shmuel
摘要： The presently disclosed subject matter includes a method, apparatus and computer storage device for reducing dispersion of a rocket caused by jet-stream misalignment, the rocket comprising a rocket engine. Information indicative of a division of total operation time of the rocket engine into a first time period and a second time period is obtained; wherein an impulse which is generated during the first time period is at least approximately the same as an impulse generated during the second time period; a period of time which equals to the first time period starting from time of activation of the rocket engine is measured; upon termination of the period of time, the rocket is rotated around the rocket's longitudinal axis; and the angle of rotation measured; and the rotation is stopped once a 180° rotation is completed.
摘要翻译： 目前公开的主题包括用于减少由射流未对准引起的火箭分散的方法，装置和计算机存储装置，该火箭包括火箭发动机。 获得表示将火箭发动机的总运转时间分割为第一时间段和第二时间段的信息; 其中在所述第一时间段期间产生的脉冲至少与在所述第二时间段期间产生的脉冲大致相同; 测量等于从火箭发动机起动时间开始的第一时间段的时间段; 一段时间结束后，火箭围绕火箭的纵轴旋转; 并测量旋转角度; 一旦180°旋转完成，则转动停止。
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公开(公告)号：WO2014199162A1
公开(公告)日：2014-12-18
申请号：PCT/GB2014/051806
申请日：2014-06-12
申请人： MBDA UK LIMITED
发明人： MILLER, Lee, Douglas
CPC分类号： F41G7/008 , F41G7/2253 , F41G7/228 , F41G7/2286 , F41G7/2293 , H01Q19/191
摘要： A sensor (20) for a missile seeker includes a primary, concave, reflector (40) that is reflective to RF waves (70) and to another kind of waves (90), but that includes a transmissive region (100), through which RF waves (70) can pass. A secondary, convex, reflector (50) is reflective to RF waves (70) but transmissive, and not reflective, to the other kind of waves (90), and is arranged facing the primary reflector (40) to further reflect RF waves (70) reflected by the primary reflector (40) through the transmissive region (100) of the primary reflector (40). An RF detector (60) is arranged on the opposite side of the primary reflector (40) from the secondary reflector (50) and arranged to detect the RF waves (70) reflected by the secondary reflector (50) through the transmissive region (100) of the primary reflector (40). A second detector (80), for detecting the other kind of waves (90), is arranged on the opposite side of the secondary reflector (50) from the primary reflector (40) and is arranged to detect the other kind of waves (90) after they are reflected by the primary reflector (40) and transmitted through the secondary reflector (50).
摘要翻译： 用于导弹探测器的传感器（20）包括对RF波（70）反射的主反射器（40）和另一种波（90），但是包括透射区域（100），通过该传感器 RF波（70）可以通过。 次级凸起的反射器（50）反射到RF波（70），但是对另一种波（90）是透射的而不是反射的，并且被布置成面向初级反射器（40）以进一步反射RF波 70）通过主反射器（40）的透射区域（100）被初级反射器（40）反射。 RF检测器（60）布置在主反射器（40）的与第二反射器（50）相反的一侧上，并布置成通过透射区域（100）检测由次级反射器（50）反射的RF波（70） ）的主反射器（40）。 用于检测另一种波形（90）的第二检测器（80）布置在第二反射器（50）的与主反射器（40）相反的一侧，并且被布置成检测另一种波（90 ）在它们被主反射器（40）反射并被透射通过次级反射器（50）之后。
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公开(公告)号：WO2014126620A1
公开(公告)日：2014-08-21
申请号：PCT/US2013/070523
申请日：2013-11-18
CPC分类号： H01L27/14625 , F41G7/008 , F41G7/2253 , F41G7/226 , F41G7/2293 , G01S3/781 , G01S3/784 , G02B26/0875 , G02B26/10 , H04N5/33 , H04N5/335
摘要： A digitally scanned multi-cell EO sensor comprises a low-resolution multi-cell imaging detector. An array of optical focusing elements decomposes the sensor's FOV into at least four sub-fields. A sub-field directing array and focusing optic direct the optical radiation onto the imaging detector. In a first tilt mode, the optical radiation from the sub-fields is directed into at least four spatially separated sub-regions that each map to a different detector cell. A high-resolution spatial light modulator (SLM) digitally scans the FOV to select different portions of the FOV to map onto the different detector cells to time demultiplex spatially overlapping portions of the FOV onto each detector cell to stitch together a sub-image of a selected area of the FOV up to the native resolution of the SLM.
摘要翻译： 数字扫描多单元EO传感器包括低分辨率多单元成像检测器。 一组光聚焦元件将传感器的FOV分解成至少四个子场。 子场引导阵列和聚焦光学器件将光辐射引导到成像检测器上。 在第一倾斜模式中，来自子场的光辐射被引导到至少四个空间上分离的子区域，每个子区域映射到不同的检测器单元。 高分辨率空间光调制器（SLM）数字扫描FOV以选择FOV的不同部分以映射到不同的检测器单元上，以将FOV的空间重叠部分时间解复用到每个检测器单元上，以将一个子图像 FOV的选定区域达到SLM的原始分辨率。
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公开(公告)号：WO2013167236A1
公开(公告)日：2013-11-14
申请号：PCT/EP2013/001179
申请日：2013-04-20
发明人： BARENZ, Joachim
CPC分类号： F41G7/008 , F41G7/2213 , F41G7/2253 , F41G7/226 , F41G7/2293 , G02B13/146 , G02B17/0808 , G02B26/108
摘要： Die Erfindung geht aus von einem Suchkopf (4) für einen Lenkflugkörper (2) mit einem bildgebenden Detektor (20), einer eine Eintrittsapertur aufweisende Optikeinheit (6) zum Abbilden eines Zielobjekts in einer Objektszene (18) auf den Detektor (20) und einem Prozessmittel (64) zum Steuern einer Lenkung des Flugkörpers (2) anhand der Abbildung des Zielobjekts auf dem Detektor (20). Ein kompakter Dual-Mode-Suchkopf (2) kann durch einen zweiten Detektor (68) geschaffen werden, wobei die Optikeinheit (6) so ausgeführt ist, dass vom Zielobjekt ausgehende Strahlung über die gleiche Eintrittsapertur der Optikeinheit (6) auf den zweiten Detektor (68) gelenkt ist, wie auf den bildgebenden Detektor (20).
摘要翻译： 本发明是基于搜索头（4），用于具有成像检测器（20），一个导弹（2），其具有（6）中的对象的场景（18）的目标对象的成像光学装置到检测器（20）的入口孔和一个 （2）基于用于控制导弹的转向处理装置（64），检测器（20）上的目标对象的图像上。 紧凑的双模式导引头（2），由第二检测器（68）被提供，其中，所述光学单元（6）被构造成使得来自所述光学单元的相同的输入孔径目标辐射出射（6）（在第二检测器上 68）被引导（如在成像检测器20）。
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