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METHOD OF ROCKET CONTROL HOMED ON LOW-ALTITUDE TARGETS

机译:以低空目标为目标的火箭弹控制方法

摘要

FIELD: methods for control of rockets designed for destruction of low-altitude targets. SUBSTANCE: an additional control command is formed for displacement of the miss expectation upwards with the use of the information on range to the underlying surface from an active pulse radio fuse. An additional command is formed in response to the information on the rate of closure to the surface produced by the inertial guidance system at the instant of appearance of the range mark to the underlying surface that is selected proceeding from the minimum allowable time of production of the additional control command before the blast of the warhead. EFFECT: enhanced antijamming capability of the guidance system, reliability and stability of its operation. 4 dwg
机译:领域:控制旨在摧毁低空目标的火箭的方法。实质:利用从有源脉冲无线电熔断器到下表面的范围信息,形成了一个附加控制命令,用于使未命中期望向上移位。响应于惯性制导系统在距离标记出现到下表面的瞬间产生的对表面的闭合率的信息,形成附加命令,该命令是从最小允许生产时间开始选择的。弹头爆炸前的附加控制命令。效果:增强了制导系统的抗干扰能力,其运行的可靠性和稳定性。 4 dwg

著录项

  • 公开/公告号RU2230281C1

    专利类型

  • 公开/公告日2004-06-10

    原文格式PDF

  • 申请/专利权人

    申请/专利号RU20020131988

  • 发明设计人 AKIMOV V.N.;

    申请日2002-11-27

  • 分类号F41G7/22;

  • 国家 RU

  • 入库时间 2022-08-21 22:45:03

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