Result Details

Simulations of Total-X based flight control system for light aircraft

CHUDÝ, P.; RZUCIDŁO, P. Simulations of Total-X based flight control system for light aircraft. Conference of Avionics. Bezmiechowa: Rzesow University of Technology, 2010. p. 1-8. ISBN: 978-83-7199-623-8.
Type
conference paper
Language
English
Authors
Chudý Peter, doc. Ing., Ph.D., MBA, DCGM (FIT)
Rzucidlo Pawel
Abstract

Thispaper discusses the design and simulation of the Total-X flight controlconcept. Total-X has been implemented into the flight control logic of a lightaircraft's flight control system. This implementation has been subjected to numeroussimulations using rapid prototyping and real-time simulation environments. Theadvantage of the Total-X system proved to be in excellent performance andmoderate complexity of the resulting controller structure compared to classicalcontrol law design.

Keywords

flight control system, light aircraft, Total-X control system, noise reduction, fuel consumption

Published
2010
Pages
1–8
Proceedings
Conference of Avionics
Conference
6th Conference in Avionics
ISBN
978-83-7199-623-8
Publisher
Rzesow University of Technology
Place
Bezmiechowa
BibTeX 
@inproceedings{BUT34398,
  author="Peter {Chudý} and Pawel {Rzucidlo}",
  title="Simulations of Total-X based flight control system for light aircraft",
  booktitle="Conference of Avionics",
  year="2010",
  pages="1--8",
  publisher="Rzesow University of Technology",
  address="Bezmiechowa",
  isbn="978-83-7199-623-8"
}
Projects
Security-Oriented Research in Information Technology, MŠMT, Institucionální prostředky SR ČR (např. VZ, VC), MSM0021630528, start: 2007-01-01, end: 2013-12-31, running
Departments
Department of Computer Graphics and Multimedia (DCGM)
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