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We developed a new method to reduce drag in aircraft by better controlling their surfaces. Our approach, based on the Lifting Line concept, efficiently allocates controls for planes with many moving parts. It minimizes drag, even if parts fail, and is adaptable to different aircraft designs. Computer simulations confirm its effectiveness and potential.

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This page is a summary of: Minimum-Drag Fault-Tolerant Aircraft Control Allocation via Online Lifting Line Calculation, Journal of Aircraft, April 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c037707.
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