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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 4: 33 - 36

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.04.034

MISSILES AND GUIDANCETECHNOLOGY

A Method of Self-optimal Aiming Control of Air-to-air Missile Interception Attack

  • SUI Yonghua ,
  • GUO Lei ,
  • YU Lixin ,
  • WANG Haiyan ,
  • OU Jianjun
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  • 1 School of Automation, Northwestern Polytechnical University, Xi'an 710072, China
    2 The Engineering Institute, Air Force Engineering University, Xi' an 710038, China

Received date: 2011-12-01

  Online published: 2025-05-29

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Abstract

To solve the problem of autonomous interception attack by using air-to-air missile for fighters, a self-optimal aiming control (SOAC) method for air-to-air missile was proposed. Firstly, the problems of autonomous interception attack were analyzed. Then, the basic idea about SOAC was introduced and the equations of aiming error were deduced. Subsequently, the model of SOAC was established and the process of SOAC was designed. Finally, the comparison experiment with the method of proportional navigation control and the robustness experiment were performed. The results show that the method of SOAC is very effective on the problems of autonomous interception attack.

Key words： air-to-air missile; autonomous attack; self-optimization; aiming control; fire control

Cite this article

SUI Yonghua , GUO Lei , YU Lixin , WANG Haiyan , OU Jianjun . A Method of Self-optimal Aiming Control of Air-to-air Missile Interception Attack[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(4) : 33 -36 . DOI: 10.15892/j.cnki.djzdxb.2012.04.034

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