Designing unmanned aerial vehicle for minimum takeoff and landing distance

In this paper, preliminary level designing of a tilt rotor UAV and tilting mechanism, are presented. Tilt rotor aircraft is a VTOL which offers more speed and comfort for payload than other VTOLs. A conceptual configuration for tilt rotor based remote controlled (RC) plane has been developed. Three...

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Bibliographic Details
Main Authors: Sreeletha, Kavya Saji, Noble, Sam, Rajaram, Dhayalan
Format: Conference Proceeding
Language:English
Subjects:
Computer simulation
Multibody systems
Tilt rotor aircraft
Unmanned aerial vehicles
Vertical takeoff aircraft
Online Access:Get full text
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Summary:In this paper, preliminary level designing of a tilt rotor UAV and tilting mechanism, are presented. Tilt rotor aircraft is a VTOL which offers more speed and comfort for payload than other VTOLs. A conceptual configuration for tilt rotor based remote controlled (RC) plane has been developed. Three tilt rotor mechanisms have been devised, modeled in CATIA V5 and analyzed with the help of the multibody dynamics simulation software ADAMS and details of the feasible mechanism were found out.
ISSN:0094-243X
1551-7616
DOI:10.1063/1.5120188