Návrh a realizace UAV se záporným šípem

Abstract

This bachelor thesis deals with the selection of a suitable concept unmanned aerial vehicle. In the introduction are analyzed the problems of concepts and according to the planned destination as unmanned aerial vehicle operating in a limited space is chosen the best conception, according to the author. The following section deals with the basic aerodynamic calculations, which is followed by the practical part, in which is appropriately chosen concept. The practical part is accompanied by a selection of suitable components and power management. In conclusion are the evaluated flight characteristics, including the measured flight data and proposed further development.