Nonlinear Model Updating of Aerospace Structures via Taylor-Series Reduced-Order Models
Nikolaos D. Tantaroudas, Jake Hollins, Konstantinos Agathos, Evangelos Papatheou

TL;DR
This paper introduces a nonlinear model updating method for aerospace structures using Taylor-series reduced-order models, effectively capturing amplitude-dependent dynamics and improving parameter accuracy.
Contribution
It combines nonlinear model order reduction with projection-basis adaptation, extending linear model updating techniques to nonlinear regimes.
Findings
Captures amplitude-dependent natural frequencies.
Improves accuracy of stiffness parameter estimation.
Outperforms purely linear updating schemes.
Abstract
Finite element model updating is a mature discipline for linear structures, yet its extension to nonlinear regimes remains an open challenge. This paper presents a methodology that combines nonlinear model order reduction (NMOR) based on Taylor-series expansion of the equations of motion with the projection-basis adaptation scheme recently proposed by Hollins et al. [2026] for linear model updating. The structural equations of motion, augmented with proportional (Rayleigh) damping and polynomial stiffness nonlinearity, are recast as a first-order autonomous system whose Jacobian possesses complex eigenvectors forming a biorthogonal basis. Taylor operators of second and third order are derived for the nonlinear internal forces and projected onto the reduced eigenvector basis, yielding a low-dimensional nonlinear reduced-order model (ROM). The Cayley transform, generalised from the real…
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