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Zexin Wang

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Open access 2026

Modeling and Integrated Control Design for Folding-Wing Aircraft during Morphing Process

ABSTRACT This paper proposes a novel integrated robust control framework tailored for folding-wing aircraft during large-angle morphing maneuvers. The morphing process induces severe nonlinearities, strong coupling between wing kinematics and vehicle dynamics, and significant time-varying shifts in the center of gravit...

Zexin Wang · 0 citations

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