Návrh UAV s kolmým startem typu křídlo

Abstract

This thesis describes the design and partial implementation of the UAV with vertical take-off type wing. The introductory chapter discusses the unmanned vehicles and their use. Other chapters deal with the following proposal wings, selected materials, components and their description. Build models, their settings, and the first flight and adjust the models work as required. At the conclusion of this thesis are inserted in Annex photographs from the implementation of a test flight.