Study on the Quick Turn Based on Reaction-jet Control of Vertical Launched Anti-tank Missile

LI  Jinping; ZENG  Wang; ZHANG  Aige; HE  Runlin

doi:10.15892/j.cnki.djzdxb.2019.02.009

Journal of Projectiles, Rockets, Missiles and Guidance >

2019 , Vol. 39 >Issue 2: 36 - 39

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2019.02.009

Study on the Quick Turn Based on Reaction-jet Control of Vertical Launched Anti-tank Missile

LI Jinping ,
ZENG Wang ,
ZHANG Aige ,
HE Runlin

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1 Xi'an Modern Control Technology Research Institute, Xi'an 710065, China
2 No. 63963 Unit, Beijing 100070, China

Received date: 2018-03-22

Online published: 2025-05-20

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Abstract

Anti-tank missile adopts the vertical ejection and the quick turn based on reaction-jet control in order to realize omnidirectional attack target, this paper innovatively presents a method of the quick turn based on reaction-jet control. First, the layout and modeling method of the pulse engine are introduced: Second, the calculation method of control deviation for quick turn is derived innovatively, and the ignition strategy of pulse engine is given in detail; Finally, the feasibility of the method of the quick turn based on reaction-jet control is verified by mathematical simulation.

Key words： vertical launch; pulse engine; reaction-jet control; quick turn

Cite this article

LI Jinping , ZENG Wang , ZHANG Aige , HE Runlin . Study on the Quick Turn Based on Reaction-jet Control of Vertical Launched Anti-tank Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019 , 39(2) : 36 -39 . DOI: 10.15892/j.cnki.djzdxb.2019.02.009

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