Návrh řízení UAV s elektropohonem

Abstract

Bachelor thesis is dealing with analysis and design of control systems for Unmanned Aerial Vehicle with Vertical Take-off and Landing characteristics. Components used for operating are described in the first part of thesis. Special emphasis is placed on stabilization systems which are important for this kind of facility. Next there is analysis and selection of contemporary control possibilities, then analysis and selection of optimal components for designed UAV. Following chapter describes complete control system and possibilities of telemetry application. Partial implementation is evidence of design accuracy.