期刊
DRONES
卷 5, 期 3, 页码 -出版社
MDPI
DOI: 10.3390/drones5030067
关键词
small unmanned aircraft systems; photogrammetry; structure-from-motion; wind impact; turbulence; crash scene reconstruction; traffic incident management
资金
- Texas Department of Transportation (TxDOT)
- Federal Highway Administration (FHWA) [0-7063]
This study uses sUAS flight simulation software to analyze the impact of wind speed, direction, and turbulence on drone flight, finding that optimal performance can be achieved when wind speed is below 11m/s and turbulence levels are light to moderate. Major lessons for real-world quadcopter sUAS flight design in windy conditions for crash scene mapping are also documented.
Small unmanned aircraft systems (sUASs) have emerged as promising platforms for the purpose of crash scene reconstruction through structure-from-motion (SfM) photogrammetry. However, auto crashes tend to occur under adverse weather conditions that usually pose increased risks of sUAS operation in the sky. Wind is a typical environmental factor that can cause adverse weather, and sUAS responses to various wind conditions have been understudied in the past. To bridge this gap, commercial and open source sUAS flight simulation software is employed in this study to analyze the impacts of wind speed, direction, and turbulence on the ability of sUAS to track the pre-planned path and endurance of the flight mission. This simulation uses typical flight capabilities of quadcopter sUAS platforms that have been increasingly used for traffic incident management. Incremental increases in wind speed, direction, and turbulence are conducted. Average 3D error, standard deviation, battery use, and flight time are used as statistical metrics to characterize the wind impacts on flight stability and endurance. Both statistical and visual analytics are performed. Simulation results suggest operating the simulated quadcopter type when wind speed is less than 11 m/s under light to moderate turbulence levels for optimal flight performance in crash scene reconstruction missions, measured in terms of positional accuracy, required flight time, and battery use. Major lessons learned for real-world quadcopter sUAS flight design in windy conditions for crash scene mapping are also documented.
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