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METHOD FOR SHAPING A MISSILE CONTROL SIGNAL WHEN GUIDING TO A MANEUVERING TARGET

机译:指导机动目标时塑造导弹控制信号的方法

摘要

FIELD: physics.SUBSTANCE: invention relates to navigation instrumentation and can be used in guidance systems for shaping a missile control signal. Technical result is higher accuracy. For this the invention comprises, for calculating a rocket control signal when guiding to a manoeuvring target, calculating reachability areas in the form of geometric figures bounded by a part of a circular arc and a curve connecting extreme points of the arc, taking into account the characteristic points of the reachability areas of the missile and manoeuvring target, and selecting control of the missile based on the position of the most distant point of the reachability area of the manoeuvring target relative to the reachability area of the missile for the selected hypothetical impact point.EFFECT: provided is increased accuracy of guiding the missile to a target, increased effectiveness of the use of missile armament when firing at high-speed and highly manoeuvrable targets while maintaining the computational complexity of the method compared with the closest analogue.1 cl, 1 dwg
机译:技术领域本发明涉及导航仪器,并且可以用于制导导弹控制信号的制导系统。技术成果是更高的精度。为此,本发明包括,为了在引导到机动目标时计算火箭控制信号,考虑到由圆弧的一部分和连接圆弧的极限点的曲线界定的几何图形形式的可到达区域,导弹和​​机动目标可到达区域的特征点,并根据选定的假设撞击点,根据机动目标可到达区域相对于导弹可到达区域的最远点的位置来选择导弹的控制效果:提供了将导弹引导至目标的精度更高,在高速和高度机动的目标射击时提高导弹武器的使用效率,同时与最接近的类似物相比保持了方法的计算复杂性。1cl, 1载重吨

著录项

  • 公开/公告号RU2017100173A3

    专利类型

  • 公开/公告日2019-01-29

    原文格式PDF

  • 申请/专利权人

    申请/专利号RU20170100173

  • 发明设计人

    申请日0000-00-00

  • 分类号F41G7/22;

  • 国家 RU

  • 入库时间 2022-08-21 11:47:12

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