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Research Article | Open Access

Learning minimum-time flight control for fixed-wing UAVs in three-dimensional space with high-fidelity 6-DOF dynamics

Guanzheng Wanga,bXiangke Wanga,bXiaoxin Lia,bZhihong Liua,b( )Zhiqiang Miaoc
College of Intelligence Science and Technology, National University of Defense Technology, Changsha, 410073, China
National Key Laboratory of Equipment State Sensing and Smart Support, National University of Defense Technology, Changsha, 410073, China
College of Electrical and Information Engineering, Hunan University, Changsha, 410012, China

Peer review under responsibility of Chongqing University.

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Abstract

Minimizing flight time while ensuring stability and efficiency presents a significant challenge in UAV control. This paper introduces velocity-level and actuator-level control approaches for addressing the minimum-time flight problem of fixed-wing UAVs, utilizing a six degrees of freedom (6-DOF) high-fidelity dynamic model and reinforcement learning. We evaluate four state-of-the-art reinforcement learning algorithms through extensive simulations and compare their performance against traditional methods. The results demonstrate that the proposed velocity-level and actuator-level control methods, based on Proximal Policy Optimization (PPO), achieve a substantial improvement in flight efficiency while maintaining strong generalization and stability. Specifically, the PPO-based actuator-level controller fully leverages the UAV’s maneuverability, resulting in a 27.6% reduction in average flight time compared to traditional controllers. The code is available as open source at https://github.com/running-mars/OpenFlight.

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Journal of Automation and Intelligence
Pages 126-138

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Cite this article:
Wang G, Wang X, Li X, et al. Learning minimum-time flight control for fixed-wing UAVs in three-dimensional space with high-fidelity 6-DOF dynamics. Journal of Automation and Intelligence, 2026, 5(2): 126-138. https://doi.org/10.1016/j.jai.2025.11.007

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Received: 29 July 2025
Revised: 05 November 2025
Accepted: 23 November 2025
Published: 24 November 2025
© 2025 The Authors.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).