您的位置: 专家智库 > >

国家自然科学基金(s60736023)

作品数:4 被引量:39H指数:3
发文基金:国家自然科学基金更多>>
相关领域:自动化与计算机技术航空宇航科学技术化学工程更多>>

文献类型

  • 2篇中文期刊文章

领域

  • 1篇自动化与计算...
  • 1篇航空宇航科学...

主题

  • 1篇时变系统
  • 1篇自适应控制
  • 1篇线性时变
  • 1篇线性时变系统
  • 1篇非线性
  • 1篇非线性时变
  • 1篇非线性时变系...
  • 1篇闭环
  • 1篇闭环系统
  • 1篇SCALE
  • 1篇CHARAC...
  • 1篇CLASS
  • 1篇COEFFI...
  • 1篇ERROR
  • 1篇MODELI...
  • 1篇ALL
  • 1篇SPACEC...
  • 1篇ATTITU...

传媒

  • 1篇Scienc...
  • 1篇Scienc...

年份

  • 1篇2010
  • 1篇2009
4 条 记 录,以下是 1-2
排序方式:
An all-coefficient adaptive control method for a class of nonlinear time-varying systems被引量:2
2009年
In this paper, the extension of the all-coefficient adaptive control method to nonlinear time-varying systems is studied. A novel discretizing method is first proposed to derive the discrete-time model for a class of nonlinear time-varying systems. The characteristics of the coefficients of the discrete-time model are derived by this method, based on which the all-coefficient adaptive control method is given for the class of nonlinear time-varying systems. Sufficient conditions on the closed-loop stability are given. Simulations show the purposed adaptive control method can achieve satisfying performance. Finally further discussion on applying low-order all-coefficient adaptive control method to high order nonlinear time-varying system is given.
ZHANG GuoQi WU HongXin
关键词:非线性时变系统自适应控制闭环系统
On characteristic modeling of a class of flight vehicles'attitude dynamics被引量:11
2010年
The characteristic modeling problem of flight vehicles'attitude dynamics is considered in this paper.In terms of the affine nonlinear system with triangle form of flight vehicles'attitude dynamics,a general method is presented to compress the dynamics into the characteristic model parameters,by introducing the time scale of nonlinear systems and a class of system states related compress functions.The parameter region and limit of the characteristic model are also given.From the given parameter region it is seen that the bound of the characteristic model parameters is dependent on the sampling period,the modeling error,the system order and the system change rate.The modeling error of the established characteristic model can be arbitrarily small according to the control precision,showing the difference between the characteristic model and other model reduction methods,that is,no system information is lost using this approach.On the basis of this modeling approach,the characteristic model of the flexible satellite attitude is established,as well as the bound and limit of the parameters,which sets a theoretical foundation for characteristic model based control design of flight vehicles.
MENG Bin &WU HongXin National Laboratory of Space Intelligent Control,Beijing Institute of Control Engineering,Beijing 100190,China
关键词:CHARACTERISTICMODELINGMODELINGERRORSCALESPACECRAFTATTITUDE
共1页<1>
聚类工具0