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http://www.scirp.org/journal/PaperInformation.aspx?PaperID=51318#.VGRvOWfHRK0
Author(s)
There are fundamental performance compromises
between rotary-wing and fixed-wing UAVs. The general solution to address
this well-known problem is the design of a platform with some degree of
reconfigurable airframes. For critical missions (civilian or military),
it is imperative that mechanical complexity is kept to a minimum to
help achieve mission success. This work proposes that the tried-and-true
radio controlled (RC) aerobatic airplanes can be implemented as basis
for fixed-wing UAVs having both speed and vertical takeoff and landing
(VTOL) capabilities. These powerful and highly maneuverable airplanes
have non-rotatable nacelles, yet capable of deep stall maneuvers. The
power requirements for VTOL and level flight of an aerobatic RC airplane
are evaluated and they are compared to those of a RC helicopter of
similar flying weight. This work provides quantitative validation that
commercially available RC aerobatic airplanes can serve as platform to
build VTOL capable fixed-wing UAVs that are agile, cost effective,
reliable and easy maintenance.
KEYWORDS
Cite this paper
Poh, C. and Poh, C. (2014) Radio Controlled “3D
Aerobatic Airplanes” as Basis for Fixed-Wing UAVs with VTOL Capability. Open Journal of Applied Sciences, 4, 515-521. doi: 10.4236/ojapps.2014.412050.
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