Detail publikačního výsledku

Low Cost Fixed Wing UAV for Development of Control Laws

KRAUS, D.; NĚMEČEK, J.

Originální název

Low Cost Fixed Wing UAV for Development of Control Laws

Anglický název

Low Cost Fixed Wing UAV for Development of Control Laws

Druh

Stať ve sborníku v databázi WoS či Scopus

Originální abstrakt

The project is focused on the development of both simulated and real UAV platform for testing of flight control algorithms. The aim of this paper was to develop a platform that allows initial design of controllers using non-linear and linearized model of UAV in Matlab/Simulink environment. Once the controllers are designed, tuned and verified in simulation, it can then be loaded into low cost UAV platform using automated code generation. The approach was verified on real plane in real environment.

Anglický abstrakt

The project is focused on the development of both simulated and real UAV platform for testing of flight control algorithms. The aim of this paper was to develop a platform that allows initial design of controllers using non-linear and linearized model of UAV in Matlab/Simulink environment. Once the controllers are designed, tuned and verified in simulation, it can then be loaded into low cost UAV platform using automated code generation. The approach was verified on real plane in real environment.

Klíčová slova

UAV, model based design, navigation

Klíčová slova v angličtině

UAV, model based design, navigation

Autoři

KRAUS, D.; NĚMEČEK, J.

Rok RIV

2016

Vydáno

03.12.2014

ISBN

978-80-214-4817-9

Kniha

Mechatronics - Mechatronika (ME), 2014 16th International Conference on

Strany od

234

Strany do

241

Strany počet

8

BibTex

@inproceedings{BUT111202,
  author="David {Kraus} and Jakub {Němeček}",
  title="Low Cost Fixed Wing UAV for Development of Control Laws",
  booktitle="Mechatronics - Mechatronika (ME), 2014 16th International Conference on",
  year="2014",
  pages="234--241",
  doi="10.1109/MECHATRONIKA.2014.7018264",
  isbn="978-80-214-4817-9"
}