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Journal of Projectiles, Rockets, Missiles and Guidance >

2015 , Vol. 35 >Issue 6: 5 - 8

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2015.06.002

MISSILES AND GUIDANCE TECHNOLOGY

A Method of Parameter Optimization for Control System of Missile Seeker Based on ISIGHT

  • LIU Mingfeng ,
  • LYU Hongpeng ,
  • LI Jie ,
  • LI Lin ,
  • CHANG Lei ,
  • SONG Zhe
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  • No. 203 Research Institute of China Ordinance Industries, Xi'an 710065, China

Received date: 2015-01-08

  Online published: 2025-05-28

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Abstract

In order to realize optimization of all parameters for control system of missile seeker, a multi-parameter design and optimization method was proposed. With the technology of MDO, the associated model of mechanical system and that of control system of seeker were integrated based on ISIGHT, and time-error integral (ITAE) was adopted for optimization, parameter optimization was carried out for control system of seeker using multi-island genetic algorithm. The results of simulation demonstrate that performance of control system of seeker has been improved by this method, which shows that this method is promising for application.

Key words： control system; multi-parameter optimization; MIGA optimization; ISIGHT

Cite this article

LIU Mingfeng , LYU Hongpeng , LI Jie , LI Lin , CHANG Lei , SONG Zhe . A Method of Parameter Optimization for Control System of Missile Seeker Based on ISIGHT[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(6) : 5 -8 . DOI: 10.15892/j.cnki.djzdxb.2015.06.002

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