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Journal of Projectiles, Rockets, Missiles and Guidance >

2017 , Vol. 37 >Issue 4: 128 - 132

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2017.04.030

CORRELATION TECHNOLOGY

Multi-source Information Fusion Navigation Technology for Unmanned Aerial Vehicle Platform

  • WANG Yukun ,
  • JIANG Liang ,
  • LIU Zhuanghua ,
  • YANG Hongxi ,
  • HUANG Bingsheng
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  • Beijing Aerospace Unmanned Aerial Vehicle System Engineering Research Institute, Beijing 100094, China

Received date: 2016-11-23

  Online published: 2025-05-28

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Abstract

In order to meet the navigation requirements of unmanned aerial vehicles(UAV), a new multi-source information fusion navigation scheme was proposed. This scheme took pseudo range and pseudo range differential information, difference information between inertial navigation and magnetic heading, difference information between height of inertial navigation and altitude of air pressure as observed quantity. The car tests showed that this system could provide reliable navigation information, and it could well solve the shortcomings that the heading error angle could not be estimated in traditional integrated navigation system engineering and the combination effect was poor in 3 star state. The results could provide references for the selection and design of UAV platform navigation scheme.

Key words： multi-source information fusion; inertial navigation; unmanned aerial vehicles platform; satellite navigation

Cite this article

WANG Yukun , JIANG Liang , LIU Zhuanghua , YANG Hongxi , HUANG Bingsheng . Multi-source Information Fusion Navigation Technology for Unmanned Aerial Vehicle Platform[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017 , 37(4) : 128 -132 . DOI: 10.15892/j.cnki.djzdxb.2017.04.030

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