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Dynamic Surface Control with Nonlinear Disturbance Observer for Uncertain Flight Dynamic System

机译:不确定飞行动力学系统的非线性扰动观测器动态表面控制

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摘要

A new robust control method of a nonlinear flight dynamic system with aerodynamic coefficients and external disturbance has been proposed.The proposed control system is a combination of the dynamic surface control(DSC)and the nonlinear disturbance observer(NDO).DSC technique provides the ability to overcome the″explosion of complexity″problem in backstepping control.NDO is adopted to observe the uncertainties in nonlinear flight dynamic system.It has been proved that the proposed design method can guarantee uniformly ultimately boundedness of all the signals in the closed-loop system by Lyapunov stability theorem.Finally,simulation results show that the proposed controller provides better performance than the traditional nonlinear controller.

著录项

  • 来源
    《南京航空航天大学学报(英文版)》 |2015年第4期|469-476|共8页
  • 作者单位

    Equipment Management and Safety Engineering College,Air Force Engineering University,Xi'an 710051,P.R.China;

    Equipment Management and Safety Engineering College,Air Force Engineering University,Xi'an 710051,P.R.China;

    Institute of Cyber-Systems and Control,Zhejiang University,Hangzhou 310027 ,P.R.China;

    Unit 93286,People's Liberation Army,Shenyang 110141,P.R.China;

  • 收录信息 中国科学引文数据库(CSCD);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 自动控制、自动控制系统;
  • 关键词

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