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Method for fuze-timing an ammunition unit, and fuze-timable ammunition unit

机译:引信定时弹药的方法和引信定时弹药的单元

摘要

The invention is based on the concept of providing a digital data transmission of the fuze-timing data into a fuze-timable ammunition unit, for example with an HDB-3 (High-Density Bipolar) transmission code and voltage modulation. As is known from asynchronous data transmission, a start byte and a stop byte are respectively positioned in front of and behind the HDB-3 code, and are therefore components of thee fuze-timing data. The fuze-timing time is transmitted numerically as a data byte between the start and stop bytes.;Accordingly, the ammunition unit (3) includes fuze-timing electronics (4), which comprise a (voltage) demodulator (30), a (current) modulator (31) and a microprocessor (32) having an RC-oscillator cycle counter (32.1), an RC oscillator (33), a fuze-timing counter (34) and an actuator end stage (36). A firing sensor (35) serves as the fuze-timing-time triggering element at the start of the flight phase. Additionally, operating data of the oscillator (33) are corrected, so simple RC oscillators can be used.
机译:本发明基于这样的概念,即例如通过HDB-3(高密度双极)传输代码和电压调制,将引信时机数据输入引信时机数据中。从异步数据传输中可以知道,起始字节和终止字节分别位于HDB-3代码的前面和后面,因此是引信定时数据的组成部分。引信计时时间以数字字节的形式在起始字节和结束字节之间传输。因此,弹药单元( 3 )包括引信计时电子设备( 4 ) ,包括(电压)解调器( 30 ),(电流)调制器( 31 )和具有RC的微处理器( 32 )振荡器周期计数器( 32.1 ),RC振荡器( 33 ),引信定时计数器( 34 )和执行器末级( 36 )。在飞行阶段开始时,点火传感器( 35 )用作引信计时时间触发元素。此外,振荡器( 33 )的操作数据已得到校正,因此可以使用简单的RC振荡器。

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