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Journal of Projectiles, Rockets, Missiles and Guidance >

2010 , Vol. 30 >Issue 2: 4 - 6

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.02.068

MISSILES AND GUIDANCE TECHNOLOGY

Proportional Navigation System with Noise Simplification Study

  • ZHANG Feiyu ,
  • QI Zaikang
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  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081,China

Received date: 2009-05-26

  Online published: 2025-05-28

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Abstract

By introducing non-dimensional method and unitary transformation to the guidance loop, the proportional navigation system with angle noise and target glint was simplified. Combining with the statistics method adjoint method, the statistic effect of homing system's parameters on guidance precision was analyzed. These conclusions are significant to proportional navigation law design.

Key words： PNG; angle noise; glint; non-dimensional; adjoint method

Cite this article

ZHANG Feiyu , QI Zaikang . Proportional Navigation System with Noise Simplification Study[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(2) : 4 -6 . DOI: 10.15892/j.cnki.djzdxb.2010.02.068

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