期刊文献+

Flutter Control of a Two-dimensional Airfoil Using Wash-out Filter Technique 被引量:3

基于Wash-out滤波器技术的机翼颤振控制(英文)
在线阅读 下载PDF
导出
摘要 The wash-out filter (WF) technique is used to control the flutter of a two dimensional airfoil with cubic non-linearity in incompressible flow. Firstly, Hopf bifurcation theory is used to determine the point at which the nonlinear controller is introduced. The system is then transformed into Jordan canonical form, based on analysis of linearized eigenvalues of the system. Secondly, for the introduced WF controller, the linear control gain is determined according to Hopf bifurcation condition. The sym- bolic computing program of normal form direct method (NFDM) is also used to obtain the normal form of the controlled system. The non-linear control gain can be determined based on the relation of the type of bifurcation and the parameters of the normal form, to transform sub-critical Hopf bifurcation to be su- per-critical one. Lastly, numerical simulations are used to certify the validity of theoretical analysis, in which the amplitude of flutter or limit cycle of the controlled system is reduced greatly, comparing to the original system. The wash-out filter (WF) technique is used to control the flutter of a two dimensional airfoil with cubic non-linearity in incompressible flow. Firstly, Hopf bifurcation theory is used to determine the point at which the nonlinear controller is introduced. The system is then transformed into Jordan canonical form, based on analysis of linearized eigenvalues of the system. Secondly, for the introduced WF controller, the linear control gain is determined according to Hopf bifurcation condition. The sym- bolic computing program of normal form direct method (NFDM) is also used to obtain the normal form of the controlled system. The non-linear control gain can be determined based on the relation of the type of bifurcation and the parameters of the normal form, to transform sub-critical Hopf bifurcation to be su- per-critical one. Lastly, numerical simulations are used to certify the validity of theoretical analysis, in which the amplitude of flutter or limit cycle of the controlled system is reduced greatly, comparing to the original system.
作者 丁千 王冬立
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2005年第2期130-137,共8页 中国航空学报(英文版)
基金 NationalNaturalScienceFoundationofChina(10272078)
关键词 nonlinear airfoil flutter control wash-out filter (WF) Hopf bifurcation normal form direct method (NFDM) nonlinear airfoil flutter control wash-out filter (WF) Hopf bifurcation normal form direct method (NFDM)
  • 相关文献

参考文献5

二级参考文献27

  • 1江俊,徐健学.动力系统的胞化积分轨迹法[J].振动工程学报,1993,6(2):194-198. 被引量:5
  • 2Ott E,Grebogy and York J A .1990 Phys Rev Lett. 64 1196.
  • 3Chert G and Dong X. 1993 IEEE Transactions on Circuits System -I 40 591.
  • 4Chen G Chaos. 1997 Soltons and Fractals , 8 1461.
  • 5Li Z and Han C Z. 2001 Chin Phys . 10 494.
  • 6Li L X, et al .2001 Chin Phys. 10 796.
  • 7Anderson P M and Fouad A A. 1977 Power System Control and Stability (Ames,IA:Iowa State University Press ).
  • 8Stevens B L and Lewis F L .1992 Aircraft Control and Simulation (New York : Wiley).
  • 9Wang H O and Abed E H .1995 Automatica 31 1213.
  • 10Chen G and Ueta T .1999 Int J Bifurcation and Chaos 9 1465.

共引文献36

同被引文献45

引证文献3

二级引证文献31

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部