Design and implementation of a VTOL flight transition mechanism and development of a mathematical model for a tilt rotor UAV
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Show full item recordDate of publishing
2018Type of publication
research articleSubject(s)
UNMANNED AERIAL VEHICLE (UAV)
HYBRID UAV MATHEMATICAL MODEL
TRI-ROTOR
FIXED-WING
VERTICAL TAKEOFF AND LANDING (VTOL)
HYBRID UAV MATHEMATICAL MODEL
TRI-ROTOR
FIXED-WING
VERTICAL TAKEOFF AND LANDING (VTOL)
Abstract
In the last decade, the interest in the development of unmanned aerial vehicles and the implementation of different flight topologies have been justified mainly by a wide range of applications, both military and civil. The current work can be used for educational purposes and we present two approaches in this area.