Research

Paper

TESTING March 17, 2026

Rapid Worst-Case Gust Identification for Very Flexible Aircraft Using Reduced-Order Models

Authors

Nikolaos D. Tantaroudas, Andrea Da Ronch, Ilias Karachalios, Kenneth J. Badcock

Abstract

Identification of worst-case gust loads is a critical step in the certification of very flexible aircraft, yet the computational cost of nonlinear full-order simulations renders exhaustive parametric searches impractical. This paper presents a reduced-order model (ROM) based methodology for rapid worstcase gust identification that achieves computational speedups of up to 600 times relative to full-order nonlinear simulations. The approach employs nonlinear model order reduction via Taylor series expansion and eigenvector projection of the coupled fluid-structure-flight dynamic system. Three test cases of increasing complexity are considered: a three-degree-of-freedom aerofoil (14 states, worst-case identified from 1,000 design sites), a Global Hawk-like UAV (540 states, 80 parametric calculations with 30 times speedup), and a very flexible flying-wing (1,616 states, 37 parametric calculations reduced from 222 hours to 22 minutes). The linear ROM is shown to be accurate for deformations below 10% of the wingspan, while the nonlinear ROM with second-order Taylor expansion accurately captures the large-deformation regime. The methodology provides a practical tool for integrating worst-case gust search into aircraft certification workflows.

Metadata

arXiv ID: 2603.16212
Provider: ARXIV
Primary Category: cs.CE
Published: 2026-03-17
Fetched: 2026-03-18 06:02

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Raw Data (Debug)
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