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Publishing Language: Chinese

Real-time landing distance prediction for aircraft based on fuzzy inference

Xi HUANG1Haogang ZHAO2Yuan XUE2Hong YANG3Huixin LIU1Pengyuan QI1( )
School of Automation Science and Electrical Engineering,Beihang University,Beijing 100191,China
The First Aircraft Institute,Aviation Industry Corporation of China,Ltd.,Xi’an 710089,China
Shanghai Aircraft Design and Research Institute,Commercial Aircraft Corporation of China,Ltd.,Shanghai 201210,China
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Abstract

A hybrid landing distance prediction algorithm based on fuzzy inference is suggested to overcome the shortcomings of current approaches in real-time performance and handling nonlinear dynamics in order to successfully prevent runway excursion incidents during aircraft landings. The method integrates multiple prediction strategies based on the three distinct dynamic phases of the landing process: during the glide phase, a ground speed vector mapping method is used for prediction; during the rollout phase, a trajectory analysis method is employed; and during the flare phase, which involves significant state changes and is difficult to model accurately, a Mamdani-type fuzzy inference method is applied. A high-fidelity simulation platform for multi-condition validation is also proposed. With a prediction inaccuracy of fewer than 35 meters during the flare phase and a computation time of less than 3 milliseconds per calculation, this platform can deliver real-time landing distance forecasts in turbulent wind environments. The proposed method meets real-time decision-making requirements and offers a feasible engineering strategy to enhance landing safety margins.

CLC number: V328;V271 Document code: A Article ID: 1001-5965(2026)08-2899-13

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Journal of Beijing University of Aeronautics and Astronautics
Pages 2899-2911

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Cite this article:
HUANG X, ZHAO H, XUE Y, et al. Real-time landing distance prediction for aircraft based on fuzzy inference. Journal of Beijing University of Aeronautics and Astronautics, 2026, 52(8): 2899-2911. https://doi.org/10.13700/j.bh.1001-5965.2025.0683

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Received: 26 September 2025
Published: 25 November 2025
© Journal of Beijing University of Aeronautics and Astronautics