Conceptual Design of a Cargo UAV That Can Take-off and Land Vertically
3rd International Congress on Human-Computer Interaction, Optimization and Robotic Applications, HORA 2021, Ankara, Turkey, 11 - 13 June 2021, (Full Text)
- Publication Type: Conference Paper / Full Text
- Doi Number: 10.1109/hora52670.2021.9461393
- City: Ankara
- Country: Turkey
- Keywords: aircraft, cargo, conceptual design, Unmanned aerial vehicle (UAV), vertical take-off and landing (VTOL)
- Dokuz Eylül University Affiliated: Yes
Abstract
Fixed-wing vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV)s are designed to combine the advantages of multi-rotor UAVs and fixed-wing UAVs in different flight phases in a single UAV. Fixed-wing VTOL UAVs can achieve the mobility of multi-rotor UAVs in hovering, vertical take-off and landing flight phases. Since fixed-wing UAVs are known for their efficiency in power consumption, fixed-wing VTOL UAVs were created to efficiently perform the cruise phase of the flight for a similar reason. In this paper, we made the conceptual design of a fixed-wing VTOL UAV which is called 'DOGA'. The mission of DOGA is to carry 0.5 kg. payload. Firstly, maximum take-off weight was calculated, and then the airfoil profile, wings geometry, and the propulsion systems were determined. Also, design and performance parameters of DOGA were calculated. As a result, conceptual design of DOGA was completed and all the needed parameters for the detail design of the fixed-wing VTOL UAV were derived.