Paper
28 August 2024 Estimation of aerodynamic parameters for a certain type of unmanned aerial vehicle
Jinhui Ge, Renjun Zhan
Author Affiliations +
Proceedings Volume 13251, Ninth International Conference on Electromechanical Control Technology and Transportation (ICECTT 2024); 132511A (2024) https://doi.org/10.1117/12.3039498
Event: 9th International Conference on Electromechanical Control Technology and Transportation (ICECTT 2024), 2024, Guilin, China
Abstract
In the process of accelerating a certain UAV to take off, the elevation angle of the launcher needs to be adjusted according to the aerodynamic characteristics of the UAV. The aerodynamic characteristics of the UAV affect the kinetic analysis of the launching process, and in order to ensure that the UAV can take off smoothly and at a predetermined speed, it is necessary to find the optimal launching angle of the launcher to provide data support for the launching kinetic simulation. In this paper, a simple aerodynamic estimation of a certain UAV is carried out based on CFD software, and the amount of calculation is reduced by simplifying the model and the calculation process, and the aerodynamic performance parameters of the UAV are finally obtained through simulation.
(2024) Published by SPIE. Downloading of the abstract is permitted for personal use only.
Jinhui Ge and Renjun Zhan "Estimation of aerodynamic parameters for a certain type of unmanned aerial vehicle", Proc. SPIE 13251, Ninth International Conference on Electromechanical Control Technology and Transportation (ICECTT 2024), 132511A (28 August 2024); https://doi.org/10.1117/12.3039498
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KEYWORDS
Unmanned aerial vehicles

Aerodynamics

Computational fluid dynamics

Computer simulations

Turbulence

Fluid dynamics

Resistance

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