Journal
AEROSPACE SCIENCE AND TECHNOLOGY
Volume 92, Issue -, Pages 635-643Publisher
ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
DOI: 10.1016/j.ast.2019.06.038
Keywords
UAV; Unmanned aerial vehicle; Multirotor; Design; Optimization
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Funding
- University of Auckland through a Faculty Research Development Fund grant
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The ability of multirotor UAVs to hold position accurately in a turbulent wind environment is important for a variety of commercial applications. In this work, a tilted-rotor configuration which offers the potential for improved disturbance rejection capability over traditional multirotor designs is presented, along with a design process to select optimal design parameters and components for a particular payload and hover time. The design process integrates models of UAV components and performance based off manufacturer data, and is applied to a range of payloads to explore resulting designs and trends. From the components considered used in this work, the tilted-rotor concept is found to provide the most benefit at payloads under 10 kg, and negligible benefit at payloads above 12 kg. (C) 2019 Elsevier Masson SAS. All rights reserved.
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