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METHOD OF FIRING JET PROJECTILES MULTIPLE ARTILLERY ROCKET SYSTEM IN COUNTER-BATTERY CONDITIONS

机译:反击条件下的多发火炮火箭系统射击方法

摘要

FIELD: military equipment.;SUBSTANCE: invention relates to military equipment and can be used in jet valley fire systems (MARS). Method comprises guiding launcher (L) in horizontal plane in direction of target, lifting guides with rocket missiles (RS) through preset angle starting in vertical plane (VP), estimating time (WS) of flight in system of independent flight path correction (SAKT) PC at initial section of path, including solid rocket engine start is PC at small angle in the IP at initial section of flight trajectory (UTV) PC taking into account technical characteristics of PU and relief arrangement PU, PC is transferred to a new path with large angle in VP after expiry of WS considering conditions of non-detection PC at initial section of trajectory of radar station counter-battery control (CBS) of enemy PC is launched with subsequent according to preset flight ballistic trajectory, simulating start of PC of fictitious point spaced from LS at a safe distance, excluding damage PU enemy artillery fire by results of locating radar station CBS start position MARS controlled pitch and yaw angles PC with help of gas-dynamic rudders by commands from SAKT PC depending on safe flight altitude of PC, which prevents detection by radar CBS, removal of PU from radar station from front line, minimum angle of view of radar station CBS branch of apparent start angle, angle of start PC branch PC speed vector angle corrections to angle of start PC, PC flight speed, permissible overload PC branch of free fall acceleration, hit target.;EFFECT: higher efficiency of firing MARS.;1 cl, 2 dwg
机译:技术领域本发明涉及军事装备,并且可以用于喷射谷火系统(MARS)。该方法包括在目标的水平平面上引导发射器(L),在垂直平面(VP)上从预设角度出发用火箭导弹(RS)抬起导管,在独立飞行路径校正(SAKT)系统中估计飞行时间(WS) )路径的初始部分(包括固体火箭发动机启动)的PC是飞行轨迹(UTV)初始部分中IP的小角度PC,考虑了PU和释放装置PU的技术特征,PC被转移到新路径WS到期后,考虑到未检测到PC的条件,在WS到期后在VP中以大角度飞行敌方PC的反电池控制(CBS)轨迹的初始部分被发射,随后根据预设的飞行弹道轨迹,模拟了PC的启动与LS保持一定距离的虚拟点,通过定位雷达站CBS起始位置MARS控制俯仰角和偏航角PC的结果,排除了对PU敌方火炮造成的伤害根据PC的安全飞行高度,通过SAKT PC发出的指令来控制气动舵,这将防止雷达CBS进行检测,从前线从雷达站移除PU,雷达站CBS的最小视角(视在起始角度,角度)启动PC分支PC速度矢量角度校正到启动PC的角度,PC飞行速度,自由落体加速度的允许过载PC分支,命中目标。;效果:发射火星的效率更高; 1 cl,2 dwg

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