Global Description of Flutter Dynamics via Koopman Theory
Jiwoo Song, Daning Huang
TL;DR
The paper tackles nonlinear aeroelastic flutter by adopting a global linearization approach based on Koopman theory. It introduces the Extended Koopman Bilinear Form (EKBF) to capture higher-order dependence on flutter parameters and demonstrates that EKBF can interpolate and extrapolate principal eigenvalues, predict flutter boundaries, and reveal nonlinear stability features via isostables and isochrons. The methodology is validated on a 2D academic model and a nonlinear panel flutter problem, showing robustness to noise and advantages over traditional AR approaches. The work provides a unified framework that connects Koopman eigenstructure with pre-flutter and post-flutter behavior, yielding practical tools for flutter analysis and prediction with actionable filtering and lifting strategies.
Abstract
This paper presents a novel parametrization approach for aeroelastic systems utilizing Koopman theory, specifically leveraging the Koopman Bilinear Form (KBF) model. To address the limitations of linear parametric dependence in the KBF model, we introduce the Extended KBF (EKBF) model, which enables a global linear representation of aeroelastic dynamics while capturing stronger nonlinear dependence on, e.g., the flutter parameter. The effectiveness of the proposed methodology is demonstrated through two case studies: a 2D academic example and a panel flutter problem. Results show that EKBF effectively interpolates and extrapolates principal eigenvalues, capturing flutter mechanisms, and accurately predicting the flutter boundary even when the data is corrupted by noise. Furthermore, parameterized isostable and isochron identified by EKBF provides valuable insights into the nonlinear flutter system.
