2022
DOI: 10.3390/app12147059
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A Small UAV Optimized for Efficient Long-Range and VTOL Missions: An Experimental Tandem-Wing Quadplane Drone

Abstract: Most types of Unmanned Aerial Vehicle (UAV, drone) missions requiring Vertical-Take-Off-and-Landing (VTOL) capability could benefit if a drone’s effective range could be extended. Example missions include Search-And-Rescue (SAR) operations, a remote inspection of distant objects, or parcel delivery. There are numerous research works on multi-rotor drones (e.g., quadcopters), fixed-wing drones, VTOL quadplanes, or tilt-motor/tilt-wing VTOLs. We propose a unique compact VTOL UAV optimized for long hover and long… Show more

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Cited by 21 publications
(13 citation statements)
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“…We attempted to keep the variables, including the aircraft weight, the cruise speed, the wing area, the wing planform design, horizontal and vertical stabilizer volume coefficient, fuselage geometry, and the forward propulsion system intake and exhaust geometry the same in all configurations. The following arm configurations were used in the comparison: a. Quad-plane [6]; b. Twin-tail boom [7][8][9]; c. Tandem wing [10,11]; d. Transverse arm.…”
Section: Methodsmentioning
confidence: 99%
“…We attempted to keep the variables, including the aircraft weight, the cruise speed, the wing area, the wing planform design, horizontal and vertical stabilizer volume coefficient, fuselage geometry, and the forward propulsion system intake and exhaust geometry the same in all configurations. The following arm configurations were used in the comparison: a. Quad-plane [6]; b. Twin-tail boom [7][8][9]; c. Tandem wing [10,11]; d. Transverse arm.…”
Section: Methodsmentioning
confidence: 99%
“…fuselage, wings, tail, etc.) is made of fiberglass and carbon fiber with wooden and carbon plates supporting the structure, which is a common technique [ 24 ]. This particular platform was chosen because of its parameters and flexibility for modifications.…”
Section: Architecture Of Uav Systemsmentioning
confidence: 99%
“…Many systems based on these platforms are designed for this task, Refs. [ 22 , 23 ] and many others take this application into account during the development process [ 24 ]. In addition to the advances in data acquisition and processing in particular applications, a UAV’s performance in the task universally depends on its parameters and ability to follow the system’s commands.…”
Section: Introductionmentioning
confidence: 99%
“…Optimization of the vehicle configuration can also be considered to account for specific requirements of the mission. Optimized for long hover and long-range missions, a new tandem-wing quadplane UAV configuration is proposed in [5].…”
Section: Vehicle Design and Characterizationmentioning
confidence: 99%