DocumentCode
236704
Title
Low cost fixed wing UAV for development of control laws
Author
Kraus, David ; Nemecek, Jakub
Author_Institution
Fac. of Mech. Eng., Brno Univ. of Technol., Brno, Czech Republic
fYear
2014
fDate
3-5 Dec. 2014
Firstpage
234
Lastpage
241
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
aerospace control; autonomous aerial vehicles; mobile robots; telerobotics; Matlab/Simulink environment; automated code generation; control law development; controller design; flight control algorithms; low cost fixed wing UAV; real UAV platform; simulated UAV platform; Aerodynamics; Airplanes; Atmospheric modeling; Computational modeling; Mathematical model; Regulators; Trajectory; UAV; model based design; navigation;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics - Mechatronika (ME), 2014 16th International Conference on
Conference_Location
Brno
Print_ISBN
978-80-214-4817-9
Type
conf
DOI
10.1109/MECHATRONIKA.2014.7018264
Filename
7018264
Link To Document