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Open access Aug 2026

Feedforward Unsteady Lift Hysteresis Compensation of Variable Camber Wing Based on Prandtl–Ishlinskii Model

The maneuvering flight of future aircraft which employ morphing variable camber wings (VCWs) requires rapid and accurate aerodynamic regulation. However, the dynamic lift responses during fast morphing deflection exhibit unsteady hysteresis effects, hindering shape and flight control performance. This study proposes a...

Xiao-Ming Wang, Jun-Yu Chen, Hao Wang et al. · 0 citations

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