DESIGN OF MINI UAV AIRCRAFT PLATFORM FUSELAGE

Abstract

Article about diploma thesis which handle conceptual design of unmanned aerial vehicle parts, engineering of fuselage construction and manufacturing technology of composite hull components. Solves basic fuselage design based on similarity with choosed wing airfoil folowed by aerodynamical simulation, constructional solutions and strenght analysys. Involves introductory landing gear project, propulsion system and control system. Handles technological instructions for preparation and manufacturing process of composite hull components.