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MISSILES AND GUIDANCE TECHNOLOGY

The Geometry Optimization of an Over-the-horizon Navigation System

  • ZHANG Junchang ,
  • SHENG Hu ,
  • WANG Guohua ,
  • ZHOU Jingwen
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  • 1 Communication Military Representative Office of Navy in Beijing Area, Beijing 100841,China
    2 Artillery Academy of PLA, Hefei 230031, China

Received date: 2009-11-15

  Online published: 2025-05-30

Abstract

GPS Navigation system plays an important role in reality, but its limited usability and discontinuous navigation capacity make it unfavorable for future use. To solve these problems, a new over-the-horizon navigation system which consists of three geo-stationary satellites and an aerostat was proposed. The optimization of constellation geometry for this system was also discussed based on minimum probability ellipsoid volume principle. Simple and effective constellation geometry was proposed after theoretic derivation. Simulation results verify the conclusion. This constellation strategy doesn't need matrix operation, thus has applicable value in reality.

Cite this article

ZHANG Junchang , SHENG Hu , WANG Guohua , ZHOU Jingwen . The Geometry Optimization of an Over-the-horizon Navigation System[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(1) : 81 -84 . DOI: 10.15892/j.cnki.djzdxb.2011.01.007

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Outlines

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