宇航计测技术 ›› 2024, Vol. 44 ›› Issue (2): 69-73.doi: 10.12060/j.issn.1000-7202.2024.02.12

• 计量保障技术 • 上一篇    下一篇

一种基于基准转换的间接瞄准测量方法

高明杰,狄世超,李发动,陈雨,王岩   

  1. 北京航天发射技术研究所,北京 100076
  • 出版日期:2024-04-15 发布日期:2024-05-01
  • 作者简介:高明杰(1976-),男,高级工程师,硕士,主要研究方向:定位定向瞄准系统设计。

An Indirect Aiming Measurement Method Based on Reference Conversion

GAO Mingjie,DI Shichao,LI Fadong,CHEN Yu,WANG Yan   

  1. Beijing Institute of Space Launch Technology,Beijing 100076,China
  • Online:2024-04-15 Published:2024-05-01

摘要: 针对无瞄准窗口的飞行器,给出一种基于基准转换的间接瞄准测量方法,通过在飞行器尾部安装基准转换装置,水平和竖直状态分别采集飞行器惯组及基准转换装置姿态信息,竖直状态通过地面捷联在激光捷联惯组上的自准直光管瞄准基准转换装置棱镜,测量其棱镜法线北向方位角,再经矩阵转换等解算得到飞行器惯组初始方位角,实现飞行器瞄准测量。

关键词: 基准转换, 瞄准测量

Abstract: An indirect aiming measurement method based on reference conversion was developed for the aircraft without aiming window. By installing a reference conversion device at the tail of the aircraft,the attitude information of the aircraft inertial measurement unit and the reference conversion device are collected in the horizontal and vertical states,and the vertical state is aimed at the prism of the reference conversion device through the ground strapdown on the laser strapdown inertial unit to obtain the northward azimuth angle of the prism,and the initial azimuth angle of the aircraft inertial measurement unit is obtained through matrix conversion and other calculations,so as to realize the aiming measurement of the aircraft. 

Key words: Reference conversion, Aiming measurement

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