Researchon Controlling Air-to-air Missile by Aerodynamic/Thrust Vector Complex Control

CHEN  Wei; WU  Xiaoyan; WU  Xiaohang

doi:10.15892/j.cnki.djzdxb.2014.03.032

Journal of Projectiles, Rockets, Missiles and Guidance >

2014 , Vol. 34 >Issue 3: 7 - 11

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2014.03.032

MISSILES AND GUIDANCE TECHNOLOGY

Researchon Controlling Air-to-air Missile by Aerodynamic/Thrust Vector Complex Control

CHEN Wei ,
WU Xiaoyan ,
WU Xiaohang

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Air and Missile Defense Collega, Air Force Engineering University, Xi'an 710051, China

Received date: 2012-05-28

Online published: 2025-05-30

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Abstract

The control method for agile turn phase of some certain air-to-air missile was investigated. The dynamic model of air-to-air missile using aerodynamic/thrust vector complex control was established. With the idea of time scale separation, the attitude kinematical and dynamical systems of the missile were divided into fast subsystem and slow subsystem. Then the control law of each subsystem was designed using the dynamic inversion control. Finally, under the condition that each portion of the missile was true, and three channels were complete coupling, simulation tests were made. The simulation shows that the control system has preferably tracking performance, and proves the correctness and effectiveness of the method.

Key words： thrust vector control; complex control; time scale separation; dynamic inversion; simulation

Cite this article

CHEN Wei , WU Xiaoyan , WU Xiaohang . Researchon Controlling Air-to-air Missile by Aerodynamic/Thrust Vector Complex Control[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(3) : 7 -11 . DOI: 10.15892/j.cnki.djzdxb.2014.03.032

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