14662

Автор(ы): 

Автор(ов): 

1

Параметры публикации

Тип публикации: 

Тезисы доклада

Название: 

Artificially created boundary crisis for aeroelastic oscillations suppression

ISBN/ISSN: 

978-88-906234-0-0

Наименование конференции: 

  • 7th European Nonlinear Dynamics Conference (ENOC 2011, Rome)

Наименование источника: 

  • Booklet of abstracts the 7th European Nonlinear Dynamics Conference (ENOC 2011, Rome)

Город: 

  • Rome

Издательство: 

  • Sapienza Università di Roma

Год издания: 

2011

Страницы: 

103
Аннотация
An active flutter suppression using saturated control is investigated for a 2dof wing section with nonlinear torsional stiffness and saturated control effectors. The suppression of oscillations in the nonlinear closed-loop system is achieved through maximization of the region of attraction for the linearized system. We study a bifurcation sequence leading to oscillating attractor destruction, which looks analogous to boundary crisis in chaotic systems. During the sequence, the boundary of attraction region touches the attractor itself before its further disappearance.

Библиографическая ссылка: 

Деменков М.Н. Artificially created boundary crisis for aeroelastic oscillations suppression / Booklet of abstracts the 7th European Nonlinear Dynamics Conference (ENOC 2011, Rome). Rome: Sapienza Università di Roma, 2011. С. 103.