Research on an Aerial Docking Strategy for Meta-UAVs Using Aerodynamic Data Surrogate Models

Meta-aircraft, in High-Altitude, Long-Endurance (HALE) unmanned aerial vehicle (UAV) applications, utilize a strategy of formation flying in the stratosphere and aerial docking in the troposphere to enhance flight range and gust resistance. This paper explores an aerial docking strategy for unmanned meta-aircraft using a surrogate model based on aerodynamic data. The study begins with an analysis of the aerodynamic characteristics and the establishment of a dynamic model, followed by the development of a surrogate model using the vortex lattice method and a BP neural network. This model accurately simulates aerodynamic changes near the wingtip. Optimization of the docking process, focusing on impulse and moment of impulse, is achieved using a greedy algorithm. The results show a reduction in drag impulse and rolling moment by 10.89% and 15.76%, respectively, thereby easing the burden on the control system of UAVs.

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Publication Details

Journal
Drones
Published
2024-12-25
DOI
https://doi.org/10.3390/drones9010007
Primary Topic
Aerospace Engineering and Control Systems
Type
article
Field-Weighted Citation Impact
0.00

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article

Research on an Aerial Docking Strategy for Meta-UAVs Using Aerodynamic Data Surrogate Models

Kangwen Sun, Xinzhe Ji, Haoquan Liang, Chenxiang Zhao et al.
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Aerospace Engineering and Control Systems
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Research on an Aerial Docking Strategy for Meta-UAVs Using Aerodynamic Data Surrogate Models

Kangwen Sun, Xinzhe Ji, Haoquan Liang, Chenxiang Zhao, Yixiang Gao, Zhiyao Wang
article en

Abstract

Meta-aircraft, in High-Altitude, Long-Endurance (HALE) unmanned aerial vehicle (UAV) applications, utilize a strategy of formation flying in the stratosphere and aerial docking in the troposphere to enhance flight range and gust resistance. This paper explores an aerial docking strategy for unmanned meta-aircraft using a surrogate model based on aerodynamic data. The study begins with an analysis of the aerodynamic characteristics and the establishment of a dynamic model, followed by the development of a surrogate model using the vortex lattice method and a BP neural network. This model accurately simulates aerodynamic changes near the wingtip. Optimization of the docking process, focusing on impulse and moment of impulse, is achieved using a greedy algorithm. The results show a reduction in drag impulse and rolling moment by 10.89% and 15.76%, respectively, thereby easing the burden on the control system of UAVs.

DronesVol. 9(1)
Beihang University (CN)
National Natural Science Foundation of China, Fundamental Research Funds for the Central Universities
Affordable and clean energy
Openalex Percentile: Top 60%
Aerospace Engineering and Control Systems
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