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METHOD FOR GUIDED MISSILE GUIDANCE ON AIR TARGET (MODIFICATIONS) AND RADAR SET FOR ITS REALIZATION

机译:空中目标(修正)导弹引导的方法及其实现的雷达集

摘要

FIELD: methods for missile radar guidance on air targets in radar guidance systems.;SUBSTANCE: guidance of missiles on an air target moving in the direction to the protected object, including the detection of the air target, evaluation of the parameters of its trajectory, missile launching, missile-to-target approach to the distance of actuation of the missile warhead blasting device, correction of the missile heading in the process of approach, blasting of the charge of the missile warhead at a distance from the protected object not less than the preset one, is accomplished in the trajectory coinciding, in the terminal leg with the predicted missile trajectory. In the terminal leg the speed of the missile is set lower than that of the air target. The result is also attained by the fact that the guidance of the missile on the air target moving in the direction to the protected object, including the detection of the air target, evaluation of the parameters of its trajectory, missile launching, missile-to-target approach to the distance of actuation of the missile warhead blasting device, correction of the missile heading in the process of approach, blasting of the charge of the missile warhead at a distance from the protected object not less than the preset one, is accomplished in the trajectory of the missile displaced in the direction to the protected object. In the terminal leg the speed of the missile is set higher than that of the air target. The result is also attained by the fact that the radar set for guidance of the missile on the air target has a missile control point and an on-board radar equipment. The missile control point includes a detection radar, a guidance radar, a computer, a servo drive, a transmitting device and an antenna device, the missile on-board equipment has a missile antenna, radio-receiving device of the missile guidance channel, actuating device, selector switch, transmitting device, radio-receiving device of the detection channel, computer.;EFFECT: reduced dynamic errors of missile guidance on an air target, and enhanced time of radio contact of the missile warhead fuse: with the air target.;5 cl, 6 dwg
机译:领域:在导弹制导系统中对空中目标进行导弹雷达制导的方法;;实质:在朝着被保护物体的方向移动的空中目标上对导弹进行制导,包括对空中目标的检测,其弹道参数的评估,导弹发射,从导弹到目标的进近以致动导弹弹头爆破装置的距离,在进近过程中校正导弹航向,在与被保护物体相距不小于预设的这一点是在轨迹一致的情况下完成的,该轨迹与终端导弹的预测轨迹相吻合。在末端,导弹的速度设定为低于空中目标的速度。通过在目标上向目标移动的导弹对空目标的制导,包括对目标的探测,对目标弹道参数的评估,导弹的发射,导弹至在以下情况下完成目标弹道:对导弹弹头爆破装置的致动距离进行瞄准;对进近过程中的导弹航向进行校正;在距被保护物体不小于预设目标的距离处对导弹弹头的装药进行爆破。导弹向受保护物体方向移动的轨迹。在末端,导弹的速度设定为高于空中目标的速度。通过用于在空中目标上引导导弹的雷达装置具有导弹控制点和机载雷达设备的事实,也可以得到结果。导弹控制点包括探测雷达,制导雷达,计算机,伺服驱动器,发射装置和天线装置,导弹机载设备具有导弹天线,导弹制导通道的无线电接收装置,致动装置装置:选择器开关,发射装置,检测通道的无线电接收装置,计算机;效果:减少导弹在空中目标上的制导动态误差,并延长导弹弹头保险丝与空中目标的无线电接触时间。 ; 5 cl,6 dwg

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