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SYSTEM FOR CONTROLLING A UNIT OF SHORT-RANGE SURFACE-TO-AIR MISSILES

机译:短距离地对空导弹控制单元的系统

摘要

The present invention pertains to the field of radiolocation techniques andmay be used in the control systems of anti-aircraft weapons. The controlsystem of the present invention comprises the following members: detectionmeans provided with an omnidirectional scanning radar; an IFF radarinterrogator; means for tracking and precisely measuring the co-ordinates ofthe target and the missile; means for displaying information; a radiotransponder; a calculator for calculating the moment when the target entersthe shooting area; an angular misalignment calculator; a range and azimuthaltracking device; a control system for the beam of the tracking radar; aprogrammable search device; a system for tracking a plurality of objectsaccording to four co-ordinates; a device for controlling the width of thedirectional characteristics of the tracking radar in the missile radiotransponder; a missile radio beacon; a tracking radar of the missile radiobeacon; a switch; and a device for recognising the type of the target and foradapting the operation modes of the missile control system.
机译:本发明涉及无线电定位技术领域,并且可用于防空武器的控制系统。控制本发明的系统包括以下成员:检测装有全向扫描雷达的装置; IFF雷达询问者跟踪和精确测量坐标的装置目标和导弹;显示信息的手段;收音机应答器用于计算目标进入时刻的计算器射击区;角度偏差计算器范围和方位角跟踪装置;跟踪雷达波束的控制系统;一种可编程搜索设备;跟踪多个物体的系统根据四个坐标;控制宽度的设备导弹无线电中跟踪雷达的定向特性应答器导弹无线电信标;导弹无线电的跟踪雷达信标开关;以及用于识别目标的类型和调整导弹控制系统的运行模式。

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