Publication 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.
Czech title
Simulace Total-X systému řízení letu pro lehké letouny
Type
conference paper
Language
English
Authors
Chudý Peter, doc. Ing., Ph.D., MBA (VZ AeroWorks)
Rzucidlo Pawel
Keywords

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

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.

Published
2010
Pages
1–8
Proceedings
Conference of Avionics
Conference
6th Conference in Avionics, Bezmiechowa, PL
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"
}
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