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SYSTEM OF HIGH-ACCURACY GUIDED HYPERSONIC ARTILLERY WEAPON

机译:高精度引导超音波武器系统

摘要

FIELD: guidance of missiles on target.;SUBSTANCE: the system has the first subsystem for determination of the target co-ordinates and output of the co-ordinate data. The second subsystem, using these data, computes the flight trajectory to the target with the mentioned co-ordinates. The projectile in such a system is launched and guided in flight in the trajectory to the target. The projectile is made in the form of a tungsten core, and the first subsystem has an infra-red imaging system of forward view and a laser range finder. The second subsystem has a fire control system. The fire control system has an additional inertial measuring device and precomputes the target co-ordinates. The projectile is installed in a rocket launched from the launching table, for example, of a launching machine. After burn-out of the rocket propellant in the initial stage the rocket launches the projectile in the flight to the target. The rocket is made in the form of a jet projectile with a guidance system and a propulsion system. The guidance system has a transceiver device installed on the projectile. The transceiver device has a low-power continuous radiator of the millimetric band. The system is installed on the launcher for an exchange of in formation with the projectile. The system on the launcher transmits short command signals to the projectile and measures the time of their passage to and fro for confirmation of the projectile range. Then the monopulse aerial installed and the launcher determines the azimuth and the elevation angle. As a result, the launcher system determines the projectile co-ordinates and its impact point. The launcher system generates a command to the projectile, which it receives and uses for the drive of the control surfaces so as to correct the projectile trajectory and the point of impact.;EFFECT: optimized operating characteristics of the guidance system and reduced cost of it.;22 cl, 3 dwg, 1 tbl
机译:技术领域:该系统具有第一个子系统,用于确定目标坐标并输出坐标数据。第二个子系统使用这些数据,使用提到的坐标来计算到目标的飞行轨迹。在这样的系统中,射弹被发射并在飞行中被引导到目标。射弹以钨芯的形式制成,并且第一子系统具有正视红外成像系统和激光测距仪。第二子系统具有火控系统。火控系统具有附加的惯性测量装置,并可以预先计算目标坐标。射弹被安装在从例如发射机的发射台发射的火箭中。在初始阶段烧尽火箭推进剂后,火箭在飞行过程中向目标发射弹丸。火箭以带有引导系统和推进系统的喷射射弹的形式制成。制导系统在射弹上安装了一个收发器设备。收发器设备具有毫米波段的低功率连续辐射器。该系统安装在发射器上,用于与射弹交换信息。发射器上的系统将短命令信号传输到弹丸,并测量它们来回穿越的时间,以确认弹丸的射程。然后安装单脉冲天线,发射器确定方位角和仰角。结果,发射器系统确定了弹丸坐标及其影响点。发射器系统向弹丸生成命令,接收并用于控制面的驱动,以校正弹丸的轨迹和撞击点。效果:优化了制导系统的操作特性并降低了其成本。; 22 cl,3 dwg,1 tbl

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