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    TÄUSCHKÖRPER
    2.
    发明申请
    TÄUSCHKÖRPER 审中-公开

    公开(公告)号：WO2019076555A1

    公开(公告)日：2019-04-25

    申请号：PCT/EP2018/075023

    申请日：2018-09-17

    Applicant: RHEINMETALL WAFFE MUNITION GMBH

    Inventor： KARAVANICH, Vikorn ,  HUBER, Florian

    IPC: F41J2/02 ,  F41J9/08 ,  F42B5/15 ,  F42B12/70

    Abstract: Vorgeschlagen wird ein Täuschkörper (3) zum Schutz eines Schnellfliegers (1) gegen eine ankommende Bedrohung (2), wobei dieser antriebslos ist. Der Täuschkörper (3) weist endseitig ein Anzündstück (6) und mündungsseitig einen Formkörper (11) auf. Besitzt der Täuschkörper (3) einen Wirkmassenbehälter (8), kann das Anzündstück (6) an diesem endseitig und der Formkörper (11) mündungsseitig an diesem angebracht werden. Das Anzündstück (6) enthält eine Treibladung, die in eine Antriebsenergie umgewandelt wird. Der Formkörper (11) ist schwerer als der Täuschkörper (3) ohne Formkörper (11) und hat die Aufgabe, das Separieren des Täuschkörpers (3) nach hinten zu verhindern. Dazu sollte der Formkörper (11) zumindest 1,0-1,5-fach schwerer sein als der Täuschkörper selbst. Vorteilhaft ist der Formkörper (11) aber doppelt so schwer.

    一种激光射击用飞靶及系统
    4.
    发明申请
    一种激光射击用飞靶及系统 审中-公开

    公开(公告)号：WO2014121482A1

    公开(公告)日：2014-08-14

    申请号：PCT/CN2013/071498

    申请日：2013-02-07

    Applicant: 马卡里

    Inventor： 马卡里

    IPC: F41J9/08 ,  F41J5/02 ,  A61F9/02

    CPC classification number: F41J5/24 ,  F41J9/08

    Abstract: 一种激光射击用的飞靶及系统，该飞靶包括：靶体（1）、柔性支架、总控制电路、导通装置和刺穿部件，所述靶体（1）由充气物体构成，围绕所述充气物体的外部轮廓设置若干柔性支架，所述柔性支架将该充气物体包围在其内；所述靶体（1）的底部和/或顶部设置激光接收器，所述激光接收器与总控制电路电连接；所述总控制电路用于根据激光接收器输入的激光编码信息，控制导通装置动作；所述导通装置与所述刺穿部件连接，所述刺穿部件在导通装置的驱动下靠近并刺穿所述充气物体。上述飞靶结构简单紧凑，击中效果明显直观，大大降低了制造成本，且应用广泛、多变，适合各种激光射击场合。

    METHOD AND FLEXIBLE APPARATUS PERMITTING ADVANCED RADAR SIGNAL PROCESSING, TRACKING, AND CLASSIFICATION/IDENTIFICATION DESIGN AND EVALUATION USING SINGLE UNMANNED AIR SURVEILLANCE (UAS) DEVICE
    5.
    发明申请
    METHOD AND FLEXIBLE APPARATUS PERMITTING ADVANCED RADAR SIGNAL PROCESSING, TRACKING, AND CLASSIFICATION/IDENTIFICATION DESIGN AND EVALUATION USING SINGLE UNMANNED AIR SURVEILLANCE (UAS) DEVICE 审中-公开

    公开(公告)号：WO2022260712A1

    公开(公告)日：2022-12-15

    申请号：PCT/US2022/011746

    申请日：2022-01-10

    Applicant: RAYTHEON COMPANY

    Inventor： WHITE, Brian, W.

    IPC: G01S7/40 ,  F41J9/08 ,  F41J2/00

    Abstract: An assembly is configured for connection to an unmanned aerial vehicle (UAV) and comprises a plurality of emulator devices each configured for attachment to the UAV and a plurality of first connection tethers each configured to operably couple a respective one of the plurality of emulator devices to the UAV at a respective spacing from the UAV. The emulator devices each comprise an emulation component configured to provide, to a target detection system, a characteristic associated with a respective type of airborne object. The plurality of respective first connection tethers each comprises material that does not substantially reflect RF energy. During flight of the UAV, when the assembly is connected, each respective emulator device maintains the respective spacing from the UAV and emulates the characteristic to the target detection system, such that the assembly emulates, to the target detection system, a plurality of airborne objects.

    SYSTEMS AND METHODS FOR PROVIDING PEER TO PEER TECHNICAL SUPPORT FOR DEVICES OVER A NETWORK
    6.
    发明申请
    SYSTEMS AND METHODS FOR PROVIDING PEER TO PEER TECHNICAL SUPPORT FOR DEVICES OVER A NETWORK 审中-公开
    用于提供对等设备的技术支持的系统和方法

    公开(公告)号：WO2017044485A1

    公开(公告)日：2017-03-16

    申请号：PCT/US2016/050549

    申请日：2016-09-07

    Applicant: 500BELOW, LLC

    Inventor： KIMBERLIN, Bill

    IPC: G09B9/02 ,  F41J9/08 ,  G09B5/14

    CPC classification number: G06Q30/016 ,  B64C39/024 ,  B64C2201/146 ,  B64D47/08 ,  B64F5/40 ,  G06Q10/063112 ,  G06Q10/10 ,  G06Q50/01 ,  G09B5/02 ,  G09B5/14 ,  G09B19/00

    Abstract: A method is described that includes receiving identification of a drone configuration from at least one user. The method includes receiving identification of training abilities from a plurality of trainers, wherein a training ability comprises an ability to provide assistance in resolving technical issues involving one or more drone configurations. The method includes receiving a training request from the at least one user for assistance in performing at least one action involving the drone configuration. The method includes identifying a trainer of the plurality of trainers with training ability applicable in assisting the at least one user in performing the at least one action. The method includes providing a training session between the at least one user and the trainer, wherein the training session comprises an electronic display simultaneously visible on a mobile device of the at least one user and a mobile device of the trainer.

    Abstract translation: 描述了一种包括从至少一个用户接收无人机配置的标识的方法。 该方法包括从多个训练者接收训练能力的识别，其中训练能力包括提供协助以解决涉及一个或多个无人机配置的技术问题的能力。 该方法包括从至少一个用户接收训练请求以帮助执行涉及无人机配置的至少一个动作。 该方法包括以适合于辅助至少一个用户执行至少一个动作的训练能力识别多个训练者的训练者。 所述方法包括在所述至少一个用户和所述训练者之间提供训练会话，其中所述训练会话包括同时在所述至少一个用户的移动设备和所述训练者的移动设备上可见的电子显示器。

    AIRCRAFT DECOY ARRANGEMENT
    8.
    发明申请
    AIRCRAFT DECOY ARRANGEMENT 审中-公开
    飞机装卸

    公开(公告)号：WO2009138983A3

    公开(公告)日：2010-03-18

    申请号：PCT/IL2009000484

    申请日：2009-05-13

    Applicant: ELBIT SYSTEMS LTD ,  ELISRA ELECTRONIC SYSTEMS LTD ,  ZAHAVI DOV ,  TANGY SHLOMO

    Inventor： ZAHAVI DOV ,  TANGY SHLOMO

    IPC: F41J2/00 ,  F41J9/08 ,  F41J9/10

    CPC classification number: F41J2/00 ,  F41G7/224 ,  F41J9/08 ,  F41J9/10

    Abstract: Aircraft decoy arrangement and method for generating a decoy signal from an aircraft having an isolated decoy. An aircraft receiver detects a threat signal from a threat source targeting the aircraft. An aircraft signal processor produces a decoy relay signal based on the threat signal, where the decoy relay signal frequency is significantly lower than the threat signal frequency and is slowly attenuated through air, the signal processor calibrating the decoy relay signal in accordance with a received test signal to compensate for inaccuracies. An aircraft transmitter transmits the decoy relay signal and an optional reference signal to the decoy, where it is received by a decoy receiver, converted back to a decoy signal by a decoy frequency converter, and transmitted by a decoy transmitter, causing the threat source to detect the decoy signal and lock onto the decoy rather than the aircraft.

    Abstract translation: 用于从具有孤立诱饵的飞行器产生诱饵信号的飞机诱饵装置和方法。 飞机接收机检测来自针对飞机的威胁源的威胁信号。 飞行器信号处理器基于威胁信号产生诱饵继电器信号，其中诱饵继电器信号频率明显低于威胁信号频率，并通过空气缓慢衰减，信号处理器根据接收到的测试校准诱饵继电器信号 信号补偿不准确。 飞行器发射器将诱饵继电器信号和可选的参考信号发射到诱饵，其中它由诱饵接收器接收，由诱饵变频器转换回诱饵信号，并由诱饵变送器发射，使得威胁源 检测诱饵信号并锁定在诱饵而不是飞机上。

    AIRCRAFT DECOY ARRANGEMENT
    9.
    发明申请
    AIRCRAFT DECOY ARRANGEMENT 审中-公开
    飞机装卸

    公开(公告)号：WO2009138983A2

    公开(公告)日：2009-11-19

    申请号：PCT/IL2009/000484

    申请日：2009-05-13

    Applicant: ELBIT SYSTEMS LTD. ,  ELISRA ELECTRONIC SYSTEMS LTD. ,  ZAHAVI, Dov ,  TANGY, Shlomo

    Inventor： ZAHAVI, Dov ,  TANGY, Shlomo

    IPC: F41J2/00 ,  F41J9/08 ,  F41J9/10

    CPC classification number: F41J2/00 ,  F41G7/224 ,  F41J9/08 ,  F41J9/10

    Abstract: Aircraft decoy arrangement and method for generating a decoy signal from an aircraft having an isolated decoy. An aircraft receiver detects a threat signal from a threat source targeting the aircraft. An aircraft signal processor produces a decoy relay signal based on the threat signal, where the decoy relay signal frequency is significantly lower than the threat signal frequency and is slowly attenuated through air, the signal processor calibrating the decoy relay signal in accordance with a received test signal to compensate for inaccuracies. An aircraft transmitter transmits the decoy relay signal and an optional reference signal to the decoy, where it is received by a decoy receiver, converted back to a decoy signal by a decoy frequency converter, and transmitted by a decoy transmitter, causing the threat source to detect the decoy signal and lock onto the decoy rather than the aircraft.

    Abstract translation: 用于从具有孤立诱饵的飞行器产生诱饵信号的飞机诱饵装置和方法。 飞机接收机检测来自针对飞机的威胁源的威胁信号。 飞机信号处理器基于威胁信号产生诱饵继电器信号，其中诱饵继电器信号频率显着低于威胁信号频率并且通过空气缓慢衰减，信号处理器根据接收到的测试来校准诱饵继电器信号 信号补偿不准确。 飞行器发射器将诱饵继电器信号和可选参考信号发射到诱饵，其中它由诱饵接收器接收，由诱饵变频器转换回诱饵信号，并由诱饵变送器发射，使得威胁源 检测诱饵信号并锁定在诱饵而不是飞机上。

    隐身大机动靶机以及隐身大机动靶机的控制方法
    10.
    发明申请
    隐身大机动靶机以及隐身大机动靶机的控制方法 审中-公开

    公开(公告)号：WO2020107846A1

    公开(公告)日：2020-06-04

    申请号：PCT/CN2019/089301

    申请日：2019-05-30

    Applicant: 北京金朋达航空科技有限公司

    Inventor： 李朝辉 ,  陈挺飞 ,  王磊 ,  孙丽君 ,  陈国峰 ,  李钊

    IPC: F41J9/08 ,  B64C3/10

    Abstract: 一种隐身大机动靶机以及隐身大机动靶机的控制方法，涉及无人飞行器技术领域，解决了现有技术中存在的靶机隐身特性差以及靶机隐身设计与飞行性能的综合匹配度不高的技术问题。该隐身大机动靶机包括机身（100）、机翼（101）、垂尾（102）、平尾（103）以及设置于机身（100）的机腹下方的"蚌式"进气道（104），机翼（101）设置于机身（100）的中部，属于下单翼布局，垂尾（102）和平尾（103）设置于机身（100）的尾部；该隐身大机动靶机的控制方法，确认高准确度、高置信度的动力学模型；采用过载和姿态组合控制，确保大过载的稳定控制飞行；控制系统使用过载、速度、攻角以及侧滑角。该隐身大机动靶机能够克服现有靶机隐身特性差的问题，并能解决靶机隐身设计与飞行性能的综合匹配度不高的问题。

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