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Journal of Projectiles, Rockets, Missiles and Guidance >

2014 , Vol. 34 >Issue 6: 25 - 28

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2014.06.007

MISSILES AND GUIDANCE TECHNOLOGY

Design and Numeric Simulation of Omni-directional Guidance Law for Infrared Air-to-air Missile

  • LI Jixin
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  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2014-02-10

  Online published: 2025-05-30

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Abstract

To satisfy the demand of omni-directional attack, omni-directional attack guidance law design is urgently needed for infrared airto-air missile. A kind of omni-directional attack guidance law based on virtual target method and large off-boresight guidance law was designed and presented in 3-D space. Performance of omni-directional attack guidance law was studied according to numerical simulation in several scenarios. Having the same form with the large off-boresight guidance law, omni-directional attack guidance law uses the same information with different sources under the condition of "over the shoulder" or "merge". Performing well under the conditions of "over the shoulder" or "merge", omni-directional attack guidance law is demonstrated to be powerful and can be applied in omni-directional attack guidance design for infrared air-to-air missile.

Key words： air-to-air missile; omni-directional attack; over the shoulder; merge; guidance law

Cite this article

LI Jixin . Design and Numeric Simulation of Omni-directional Guidance Law for Infrared Air-to-air Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(6) : 25 -28 . DOI: 10.15892/j.cnki.djzdxb.2014.06.007

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