Bp 163 en
Control systems for UAV´s
Author: Michal Padyšák
This bachelor thesis is divided into two parts. The first part is focused on the project RAMA of Department of Control Engineering, Faculty of Electrical Engineering at Czech Technical University in Prague, which purpose is to design and build a universal lightweight and compact control system for small UAV. Component of thesis is evaluation of web page of project and design controller for first layer control system of UAV helicopter. The second part of this bachelor thesis is focused on the concerted project of DCE FEE at CTU and VTUL Prague, which purpose is to development on stabilized platform for small UAV devices. There are compared properties of available microcontrollers units ATMEL for control system for stabilized platform. At the end of thesis a program project in C were designed for purposes of testing run time of algorithms for microcontroller AT91SAM7X256.
