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METHOD TO CONTROL ROCKET HIGH-EXPLOSIVE WARHEAD KILLABILITY FIELD CHARACTERISTICS AND DEVICE TO THIS END

机译:为此目的控制火箭弹高爆头可杀伤性场特性和装置的方法

摘要

FIELD: weapons and ammunition.;SUBSTANCE: proposed method consists in using two target contactless pickups operating in different ranges of electromagnetic spectrum, locking the target and defining target flight side at notable misses by target radiometric pickup, locking the target and defining target flight side at insignificant misses by target optical pickup. Firing instruction is generated by electronic unit of delay time computation. Killability field towards the target is generated by sending "go" instruction to actuator with its terminal assembly shifted towards side opposite target flight side. Additionally, target location sector with respect to rocket lengthwise axis is determined proceeding from comparison of polarity of signals from azimuth and elevation angle pickups. Target selection is performed by spatial attribute proceeding from comparison of target flight side determined by radiometric and optical pickups of target. Proposed device comprises contact target pickup, radiometric contactless pickup, optical contactless pickup, firing delay time computation unit incorporating device that generates instruction for actuator with its terminal assembly shifted towards side opposite target flight side.;EFFECT: higher noise immunity.;3 cl, 4 dwg
机译:领域:武器和弹药。实质:所提出的方法包括使用两个在不同电磁频谱范围内工作的目标非接触式拾音器,锁定目标并通过目标辐射式拾波器将目标飞行侧定义为明显失误,锁定目标并定义目标飞行侧目标光学头的微不足道的失误。触发指令由延迟时间计算的电子单元生成。通过向执行器发送“执行”指令,使其终端组件移向与目标飞行侧相反的一侧,可生成朝向目标的杀伤力场。另外,相对于火箭纵轴的目标位置扇区是通过比较来自方位角和仰角拾取器的信号极性来确定的。目标的选择是通过比较由目标的辐射度和光学拾取器确定的目标飞行侧来进行的空间属性来执行的。拟议的设备包括接触目标拾音器,辐射非接触拾音器,光学非接触拾音器,发射延迟时间计算单元,该设备结合了可为执行器生成指令的设备,其终端组件朝着与目标飞行侧相反的一侧移动;效果:更高的抗扰性; 3 cl, 4 dwg

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