Publication detail

Low Cost Fixed Wing UAV for Development of Control Laws

KRAUS, D. NĚMEČEK, J.

English title

Low Cost Fixed Wing UAV for Development of Control Laws

Type

Paper in proceedings (conference paper)

Language

en

Original abstract

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.

Keywords in English

UAV, model based design, navigation

Released

2014-12-03

ISBN

978-80-214-4817-9

Book

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

Pages from–to

234–241

Pages count

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"
}