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    • 7. 发明公开
    • METHOD AND ARRANGEMENT FOR THREAT MANAGEMENT FOR GROUND-BASED VEHICLE
    • VERFAHREN UND ANORDNUNG ZURBEKÄMPFUNGVON BEDROHUNGEN EINES BODENFAHRZEUGS
    • EP2959260A4
    • 2016-10-05
    • EP14754527
    • 2014-02-20
    • BAE SYSTEMS HÄGGLUNDS AKTIEBOLAG
    • BACKSTRÖM RONNYSVENSSON GÖSTA
    • F41H11/00F41H7/02
    • F41H11/00F41H7/02
    • The invention pertains to a method for threat handling of a ground based vehicle, comprising the steps of providing at least two kinds of systems for said threat handling, wherein said threat handling comprises determining information about said threat and determining actions for handling said threats based upon said information, and providing a control unit for controlling provided systems, providing a separate hardware safety configuration unit, and providing said separate hardware safety configuration unit with by means of provided means determined information about said threat so as to in an evaluation step deciding if said control unit should be given a go ahead for handling said threat or not. The invention also relates to a computer program product comprising program code for a computer implementing a method according to the invention. The invention also relates to a device and a ground based vehicle which is equipped with the device.
    • 本发明涉及一种用于威胁处理基于地面的车辆的方法,包括以下步骤:为所述威胁处理提供至少两种系统,其中所述威胁处理包括确定关于所述威胁的信息并且基于以下方式确定处理所述威胁的动作 并提供一个用于控制所提供的系统的控制单元,提供单独的硬件安全配置单元,并通过提供的装置提供关于所述威胁的确定的信息来提供所述单独的硬件安全配置单元,以便在评估步骤中决定是否所述 应该对控制单位进行处理,否则处理上述威胁。 本发明还涉及包括用于实现根据本发明的方法的计算机的程序代码的计算机程序产品。 本发明还涉及一种装备有该装置的装置和基于地面的车辆。
    • 8. 发明公开
    • SENSOR FOR AIRBORNE SHOOTER LOCALIZATION SYSTEM
    • 传感器FÜREIN系统ZUR LOKALISIERUNG VONSCHÜTZENIN DER LUFT
    • EP2297592A4
    • 2015-06-03
    • EP09746937
    • 2009-05-12
    • RAYTHEON BBN TECHNOLOGIES CORP
    • BARGER JAMES ESTANLEY JOHN
    • G01S3/808B64C27/04B64D7/00F41H11/00F41H13/00G01H11/00G01H11/06G01S3/86G10K11/00
    • B64D7/00B64C27/04F41H11/00F41H13/00G01H11/06G01S3/808G01S3/86G10K11/002G10K11/004H04R2410/00
    • A sensor assembly suitable for use in an airborne shooter localization system. The sensor assembly has a pressure sensor subassembly with a pressure transducer positioned to detect pressure variations associated with a shock wave from a passing projectile or the muzzle blast following the shock wave. To substantially increase the signal to noise ratio for measurements of the shock wave, the pressure sensor subassembly attenuates pressure fluctuations triggered by turbulent airflow over the surface of the subassembly more than it attenuates the shock wave. This preferential attenuation is provided by separating the pressure transducer from the surface of the sensor assembly by a cavity large enough that the pressure fluctuations are substantially attenuated as they propagate across the cavity. Additionally, features of a housing that holds the pressure sensor subassembly facilitate use on an aircraft. Those features include flexibility that allows the sensor assembly to conform to curved surfaces, a skin that provides resistance to environmental conditions and allows the sensor assembly to be attached with an adhesive, and a body region that provides high vibrational impedance to prevent low frequency mechanical vibrations from being coupled to the pressure transducer.
    • 适用于机载射手定位系统的传感器组件。 传感器组件具有压力传感器子组件,压力传感器定位成用于检测与冲击波之后的经过的射弹或枪口爆炸的冲击波相关联的压力变化。 为了大大增加用于冲击波测量的信噪比,压力传感器子组件衰减了比组件表面上的湍流气流触发的压力波动更多的是衰减冲击波。 通过将压力传感器与传感器组件的表面分开一个足够大的空腔,使压力波动在其穿过空腔传播时基本上衰减而提供这种优先衰减。 此外,保持压力传感器子组件的壳体的特征便于在飞机上使用。 这些特征包括灵活性,其允许传感器组件符合弯曲表面,提供对环境条件的抵抗力并允许传感器组件用粘合剂附着的皮肤,以及提供高振动阻抗以防止低频机械振动的身体区域 从耦合到压力传感器。