Multioutput Autoregressive Aeroelastic System Identification and Flutter Prediction
Author:
Affiliation:
1. Technion–Israel Institute of Technology, 3200000 Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034789
Reference23 articles.
1. Aeroelastic Dynamic Analysis of a Full F-16 Configuration for Various Flight Conditions
2. Nonlinear mechanisms of transonic aeroelastic instability for the F-16
3. Three-Dimensional Transonic Aeroelasticity Using Proper Orthogonal Decomposition-Based Reduced-Order Models
4. Aeroelastic System Development Using Proper Orthogonal Decomposition and Volterra Theory
5. Reduced-Order Modeling of Flutter and Limit-Cycle Oscillations Using the Sparse Volterra Series
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4. Aeroelastic System Identification for Flutter Prediction via Multi-Output Autoregressive Modeling;Journal of Aircraft;2023-12-29
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