Rigid–Elastic Coupling Dynamics of Morphing Wing Aircraft

This paper presents a rigid–elastic coupling dynamic model for a morphing aircraft with variable-sweep wings, developed using Kane’s method. The model accurately captures the interactions between flight dynamics and structural dynamics during morphing. To fully account for the coupling effects, we d...

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Bibliographic Details
Main Authors: Siyu Hua, Xugang Wang, Zhongyuan Wang
Format: Article
Language:English
Published: MDPI AG 2025-04-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/12/4/327
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