Koncepční návrh a konstrukční řešení UAV s využitím nosné plochy kruhového půdorysu

Abstract

This master thesis deals with practical usage of circular wing design in combination with a vertical takeoff and landing technology. The thesis puts focus on usage of final product as Unmaned Air Vehicle. The first part of this thesis analyzes current and common types of Unmaned Air Vehicles. The following part of this thesis describes the deignment of a concept which is using circular wing design. The last part deals with construction of Unmaned Air Vehicle which is based on final form of a concept and with flight testing.