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Journal of Projectiles, Rockets, Missiles and Guidance >

2022 , Vol. 42 >Issue 3: 5 - 10

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2022.03.002

Research on Angle Type Guidance Method for Anti-radar Missiles

  • TANG Daoguang 1 ,
  • ZHANG Yi 2 ,
  • LIU Xuhan 2 ,
  • WANG Qiao 2 ,
  • LI Tao 2 ,
  • YANG Dan 3
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  • 1 School of Electrical and Control Engineering, North University of China, Taiyuan 030051, China
  • 2 Xi’an Modern Control Technology Research Institute, Xi’an 710065, China
  • 3 Technology Center, Southwest Computer Co., Ltd., Chongqing 400060, China

Received date: 2021-11-10

  Online published: 2025-02-03

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Abstract

Based on the derivation of optimal proportional navigation, the new expressions with line of sight angle and trajectory angle for proportional navigation, integral proportional navigation and velocity pursuit are proposed. The guidance model with initial heading error is developed when considering a high order dynamics system for the integral proportional navigation and velocity pursuit. Comparative analysis results of miss distance demonstrate the guidance performance of integral proportional navigation and velocity pursuit.

Key words： anti-radar missile; guidance method; integral proportion navigation; velocity pursuit

Cite this article

TANG Daoguang , ZHANG Yi , LIU Xuhan , WANG Qiao , LI Tao , YANG Dan . Research on Angle Type Guidance Method for Anti-radar Missiles[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2022 , 42(3) : 5 -10 . DOI: 10.15892/j.cnki.djzdxb.2022.03.002

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