Online Data-Driven Optimization of Aerodynamic Performance for an Unconventional Morphing Aircraft
T. Woldhuis (TU Delft - Aerospace Engineering)
Sherry Wang – Mentor (TU Delft - Group Wang)
S. Asaro – Mentor (TU Delft - Flight Performance and Propulsion)
R Vos – Graduation committee member (TU Delft - Flight Performance and Propulsion)
Coen de Visser – Graduation committee member (TU Delft - Control & Simulation)
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Abstract
In nature, birds can intelligently adapt their wing shapes to their environment. This paper aims to replicate this capability by designing an online data-driven aerodynamic performance optimization framework for an unconventional morphing aircraft. Compared to state-of-the-art methods, the proposed framework efficiently finds global optima with reduced computational load when addressing time-varying, nonlinear, and non-convex problems. It also demonstrates enhanced adaptability to unforeseen scenarios. In the event of a sudden actuator fault, the algorithm can automatically detect the fault, adapt the onboard data-driven model, and continue performing optimization and trimming tasks using the remaining healthy actuators. Additionally, the paper addresses the optimal number of actuators within a morphing surface, considering the tradeoff between optimization performance and the weight penalty. High-fidelity simulations demonstrate that through active morphing, the proposed framework achieves drag reductions of 1.9–4.9 % during cruise and up to 12.6 % at higher operational lift coefficients (due to heavier weight and lower speed), resulting in an overall drag reduction of 2.98 % over a typical flight cycle, which corresponds to fuel savings of approximately 150 kg/h. This research represents a significant advancement in sustainable aviation, contributing to reduced fuel consumption, lower emissions, and improved fault tolerance for next-generation aircraft.
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File under embargo until 31-12-2025