Publication Details

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

CHUDÝ Peter and RZUCIDŁO Paweł. Simulations of Total-X based flight control system for light aircraft. In: Conference of Avionics. Bezmiechowa: Rzesow University of Technology, 2010, pp. 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 (DCGM FIT BUT)
Rzucidło Paweł, Ph.D. Eng. (RUT)
Keywords

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

Abstract

This paper discusses the design and simulation of the Total-X flight control concept. Total-X has been implemented into the flight control logic of a light aircraft's flight control system. This implementation has been subjected to numerous simulations using rapid prototyping and real-time simulation environments. The advantage of the Total-X system proved to be in excellent performance and moderate complexity of the resulting controller structure compared to classical control 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, PL
BibTeX 
@INPROCEEDINGS{FITPUB9264,
   author = "Peter Chud\'{y} and Pawe\l Rzucid\lo",
   title = "Simulations of Total-X based flight control system for light aircraft",
   pages = "1--8",
   booktitle = "Conference of Avionics",
   year = 2010,
   location = "Bezmiechowa, PL",
   publisher = "Rzesow University of Technology",
   ISBN = "978-83-7199-623-8",
   language = "english",
   url = "https://www.fit.vut.cz/research/publication/9264"
}
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