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弹箭与制导学报 >

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

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

导弹与制导技术

一种非最小相位导弹过载控制系统设计方法研究

  • 祝萌 ,
  • 吴晓男 ,
  • 于进勇
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  • 1 哈尔滨工程大学自动化学院,哈尔滨 150001
    2 海军航空工程学院自动控制系,山东烟台 264001

祝萌(1981-),女,山东菏泽人,硕士研究生,研究方向:飞行器控制系统设计与仿真。

收稿日期: 2009-04-27

  网络出版日期: 2025-05-19

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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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摘要

针对导弹过载控制的非最小相位系统特征,提出了一种以滑模面作为输出的滑模控制方法,该方法以反演设计和输出重定义相结合,并且通过李雅普诺夫稳定性理论证明了该方法的理论可行性。最后利用某型导弹的过载数学模型进行了数字仿真,仿真结果证明了该控制系统设计方法的有效性。

关键词： 导弹; 非最小相位系统; 李雅普诺夫稳定性; 过载控制

本文引用格式

祝萌 , 吴晓男 , 于进勇 . 一种非最小相位导弹过载控制系统设计方法研究[J]. 弹箭与制导学报, 2010 , 30(1) : 47 -50 . DOI: 10.15892/j.cnki.djzdxb.2010.01.071

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

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参考文献

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