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Journal of Projectiles, Rockets, Missiles and Guidance >

2010 , Vol. 30 >Issue 1: 47 - 50

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.01.071

MISSILES AND GUIDANCE TECHNOLOGY

Study of a Non-minimum Phase System on Missile Overload Control

  • ZHU Meng ,
  • WU Xiaonan ,
  • YU Jinyong
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  • 1 College of Automation, Harbin Engineering University, Harbin 150001,China
    2 Department of Automatic Control, Naval Aeronautical and Astronautical University,Shandong Yantai 264001, China

Received date: 2009-04-27

  Online published: 2025-05-19

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Abstract

A method which defines the sliding surface as a new output has been put forward for a non minimum phase system of missile overload, in which the methods of backstepping and output redefinition are combined. Then Lyapunov stability theorem is used to prove the correctness of the design method. Finally simulation for missile model on overload is made, and the results have shown the correctness and effectiveness of the method.

Key words： missile; non-minimum phase system; Lyapunov stability theorem; overload control

Cite this article

ZHU Meng , WU Xiaonan , YU Jinyong . Study of a Non-minimum Phase System on Missile Overload Control[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(1) : 47 -50 . DOI: 10.15892/j.cnki.djzdxb.2010.01.071

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