弹道与气动力技术

基于非线性动态逆的弹道修正控制设计研究

  • 曾耀华 ,
  • 王华 ,
  • 韩晶 ,
  • 王义宁
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  • 1 中北大学机电工程学院,太原 030051
    2 北京航空航天大学宇航学院,北京 100083

曾耀华(1985-),男,江西赣州人,硕士研究生,研究方向:机电控制、弹道修正。

收稿日期: 2009-07-14

  网络出版日期: 2025-05-28

Research on the Design of Nonlinear Dynamic Inversion Control in Trajectory Correction

  • ZENG Yaohua ,
  • WANG Hua ,
  • HAN Jing ,
  • WANG Yining
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  • 1 School of Mechatronics Engineering, North University of China, Taiyuan 030051, China
    2 School of Astronautics, BUAA, Beijing 100083, China

Received date: 2009-07-14

  Online published: 2025-05-28

摘要

为了实现强耦合的非线性二维弹道修正方程解耦控制并线性化,基于非线性逆系统原理,采用三时标分离方法,在考察系统状态变量动态特性基础上,分离系统为三子系统,然后分别对各子系统设计逆控制器,对线性化后的系统基于Lyapunov函数法设计线性控制器。最后通过Matlab仿真验证了逆系统方法的有效解耦控制,并通过选择不同的回路带宽比较了系统的动态性能,结果表明了该方法的正确性和有效性。

本文引用格式

曾耀华 , 王华 , 韩晶 , 王义宁 . 基于非线性动态逆的弹道修正控制设计研究[J]. 弹箭与制导学报, 2010 , 30(3) : 131 -134 . DOI: 10.15892/j.cnki.djzdxb.2010.03.037

Abstract

Based on nonlinear inverse system theory, the three time-scale separation method was put forward for decoupling and linearizing the strong coupling and nonlinear trajectory correction equations. On the basis of the system states dynamic characteristics, the system was separated into three subsystems. Then, the inverse system controllers were designed for these subsystems separately, and the linear controllers were also done for the linearized systems by the Lyapunov function method. Finally, with the Matlab simulation, it was verified the efficiency of the inverse system method, and compared the system's dynamic performance by selecting different loop bandwidths. The results indicate that the method is correct and effective.

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