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Journal of Projectiles, Rockets, Missiles and Guidance >

2017 , Vol. 37 >Issue 3: 1 - 4

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2017.03.001

MISSILES AND GUIDANCE TECHNOLOGY

Research on Self Adaptive Missile Spin Method

  • CAO Ercong ,
  • ZHOU Liyong ,
  • ZHU Tieyong ,
  • LIANG Xiaoyu ,
  • HU Xiaobo
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  • North Electro-Optic Co. Ltd, Xi'an 710043, China

Received date: 2016-11-13

  Online published: 2025-05-28

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Abstract

The change of projectile speed is difficult to track the target effectively. To eliminate the projectile speed changes affect seeker tracking target. An adaptive method is presented for the large range of projectile speed change. This method can not only under the projectile speed variation in real time to provide accurate information on the range, and effectively improve the efficiency of precession of seeker. Realize the seeker in the projectile spin eliminate change speed of its effects, precise tracking target, ensure the missile accuracy.

Key words： seeker; control; missile spin self; adaption

Cite this article

CAO Ercong , ZHOU Liyong , ZHU Tieyong , LIANG Xiaoyu , HU Xiaobo . Research on Self Adaptive Missile Spin Method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017 , 37(3) : 1 -4 . DOI: 10.15892/j.cnki.djzdxb.2017.03.001

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