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Anti-radiation end-of-flight homing device for missile navigation system e.g. air-to-surface missile

机译:用于导弹导航系统的防辐射飞行结束自导装置,例如空对地导弹

摘要

The antiradiation homing device guides the vehicle near to a source of radiation and an end-of-flight homing device with its own estimation of measurement quality (90) takes the vehicle to the objective. The goniometer has several antennae (30) along a side wall of the vehicle, freeing the front of vehicle for the end-of-flight homing device. The goniometer has a receiver (31) and the means to determine the direction (34) and the range (33) of the radiation sources from the direction and values held in a memory (35). An identification unit (32) identifies the source from its characteristics and a library of characteristics and a clock (36) provides to the memory the date of information so as to update information to the trajectory processor.
机译:防辐射归位装置将车辆引导至辐射源附近,而飞行结束归位装置则以其自身对测量质量的估计值(90)将车辆对准目标。测角计沿着车辆的侧壁具有多个天线(30),从而将车辆的前部释放以用于飞行结束归位装置。测角仪具有接收器(31)和用于根据保持在存储器(35)中的方向和值来确定辐射源的方向(34)和范围(33)的装置。识别单元(32)从其特征和特征库中识别源,并且时钟(36)将信息的日期提供给存储器,以便将信息更新至轨迹处理器。

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