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METHOD FOR PROTECTING ANTI-AIRCRAFT ROCKET COMPLEXES FROM ANTI-RADAR ROCKETS

机译：从反雷达火箭上防护反飞机火箭复合物的方法

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摘要

A method for protecting anti-aircraft rocket complexes from anti-radar rockets in which one detects the anti-radar rocket, follows the anti-radar rocket in automated mode or tracking, with performing pre-start operations, determining the instant of the anti-radar rocket entrance to the zone of the anti-aircraft rocket complex launch; and at the end stage, at the anti-radar rocker entering to the launch zone, one performs firing on it by the anti-aircraft rocket complex. Main point of the method is in the fact that first one determines through the tracking data additional information on the trajectory of movement of the anti-radar rocket, with implementation of operation on calculation, from the data of information on the trajectory, of the coordinates of the end point of the anti-radar rocket motion; one adjusts in time the coordinates of the anti-radar rocket motion, adjusts the coordinates of the end point of the anti-radar rocket motion, switches on the transmitter of the radar station of the anti-aircraft radar complex, with switching the radar station of the anti-aircraft complex to passive mode of operation; the rocket is followed in passive mode of operation of the radar station of the anti-aircraft radar complex at place angle and the radius only till the anti-radar rocket enters the zone of the anti-aircraft radar station launch; the entrance of the anti-radar rocket to the zone of the anti-aircraft radar station launch is controlled, and at entrance of the anti-radar rocket to the launch zone one performs its firing by the anti-aircraft rocket complex. This invention improves protection of functionally linked means of tracking and fire hitting of air targets of anti-aircraft rocket complexes in case those are attacked by antiradar rockets.

机译：一种保护防空火箭复合物免受反雷达火箭袭击的方法，其中，一个人会检测到反雷达火箭，然后以自动模式或跟踪方式跟踪反雷达火箭，执行预启动操作，确定反雷达的瞬间雷达火箭进入防空火箭综合体发射区;最后，在进入发射区的反雷达摇杆上，由防空火箭系统向其发射。该方法的要点在于，首先通过跟踪数据确定反雷达火箭的运动轨迹的附加信息，并通过计算操作，从轨迹信息中获取坐标值。反雷达火箭运动的终点;一个及时调整反雷达火箭运动的坐标，调整反雷达火箭运动的终点的坐标，打开防空雷达综合体雷达站的发射机，并切换雷达站防空综合体的运行方式为被动运行;在防空雷达综合体雷达站的被动运行模式下，以一定角度和半径跟踪火箭，直到防雷达火箭进入防空雷达站发射区为止;防空火箭进入防空雷达站发射区的入口受到控制，防空火箭进入发射区的入口由防空火箭联合体进行射击。本发明改进了防空火箭复合物的空中目标在受到反雷达火箭弹袭击时跟踪和击中空中目标的功能性连接装置的保护。

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公开/公告号UA65854A

专利类型
公开/公告日2004-04-15

原文格式PDF
申请/专利权人 MILITARY UNIT A0858;DRUZHYNIN VOLODYMYR ANATOLIIOVYCH;
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申请/专利号UA20030065434
发明设计人 DRUZHYNIN VOLODYMYR ANATOLIIOVYCH;ZAIKIVSKYI OLEKSANDR BOLESLAVOVYCH;PONOMARIOV OLEKSANDR VASYLIOVYCH;KOMAROV VOLODYMYR SERHIIOVYCH;KRYZHNYI ARKADII VOLODYMYROVYCH;KHYZHNIAK VOLODYMYR VITALIIOVYCH;KOMAROV VOLODYMYR OLEKSANDROVYCH;LUKHANIN MYKHAILO IVANOVYCH;
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申请日2003-06-11
分类号F41H11/02;F41H13/00;
国家 UA
入库时间 2022-08-21 23:08:28

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