宇航计测技术

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导弹侵切角测量方法研究

张原1,2;张晓辉1;王志乾1;乔彦峰1   

  1. 1、中国科学院长春光学精密机械与物理研究所,长春 130033;
    2、中国科学院大学,北京 100039
  • 出版日期:2015-08-15 发布日期:2015-08-15
  • 作者简介:张原(1990-),女,硕士研究生,主要研究方向:光电测量与检测方面的研究。
  • 基金资助:
    吉林省重点科技攻关资助项目(20150204013GX)

Research of Measuring Method for Missile Invaded Angle

ZHANG Yuan1,2;ZHANG Xiao-hui1;WANG Zhi-qian1;QIAO Yan-feng1   

  1. 1、Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033;
    2、University of Chinese Academy of Sciences,Beijing 100039
  • Online:2015-08-15 Published:2015-08-15

摘要: 针对导弹攻击目标时的侵切角测量问题,提出采用2台高速摄像机近距离凝视交会测量导弹中轴线上特征点位置,结合在试验前通过精密测量目标被攻击平面特征点方法建立的平面方程,分析计算侵切角。仿真结果表明:在高速摄像机测角精度优于13.4″的情况下,测量精度优于1°。该方法技术实现容易,对导弹攻击陆上目标试验时的侵切角测量,具有一定的参考价值。

关键词: 导弹试验, 姿态测量, 侵切角测量, 交会测量

Abstract: In order to measure invaded angle of the missile to attack the target, it is presented to use two High-speed camera, near distance gazed fixedly intersection measuring locations for characteristic points of missile middle axes, combining to plane equation is founded by precise measuring characteristic points of target attacked planes before test, invaded angle is calculated. The measuring accuracy could be acquired less than 1°in invaded angle by simulating result proving in these methods, if measure angle precision is less than 13.4″ in High-speed camera. The method is carried out easily in technique, gives a reference to measure invaded angle for missile test attacking land targets.

Key words: Missile test, Attitude measurement, Invaded angle measurement, Intersection measurement