1. Feedback control of a nonlinear aeroelastic system with non-semi-simple eigenvalues at the critical point of Hopf bifurcation
- Author
-
Suhuan Chen, Yudong Chen, Lina Liu, Licai Wang, and Chunyan Pei
- Subjects
Hopf bifurcation ,0209 industrial biotechnology ,Applied Mathematics ,Feedback control ,Computational Mechanics ,General Physics and Astronomy ,Statistical and Nonlinear Physics ,02 engineering and technology ,Aeroelasticity ,01 natural sciences ,Nonlinear system ,symbols.namesake ,020901 industrial engineering & automation ,Mechanics of Materials ,Critical point (thermodynamics) ,Simple (abstract algebra) ,Modeling and Simulation ,0103 physical sciences ,symbols ,Applied mathematics ,010301 acoustics ,Engineering (miscellaneous) ,Eigenvalues and eigenvectors ,Mathematics - Abstract
The feedback control of Hopf bifurcation of nonlinear aeroelastic systems with asymmetric aerodynamic lift force and nonlinear elastic forces of the airfoil is discussed. For the Hopf bifurcation analysis, the eigenvalue problems of the state matrix and its adjoint matrix are defined. The Puiseux expansion is used to discuss the variations of the non-semi-simple eigenvalues, as the control parameter passes through the critical value to avoid the difficulty for computing the derivatives of the non-semi-simple eigenvalues with respect to the control parameter. The method of multiple scales and center-manifold reduction are used to deal with the feedback control design of a nonlinear system with non-semi-simple eigenvalues at the critical point of the Hopf bifurcation. The first order approximate solutions are developed, which include gain vector and input. The presented methods are based on the Jordan form which is the simplest one. Finally, an example of an airfoil model is given to show the feasibility and for verification of the present method.
- Published
- 2021
- Full Text
- View/download PDF