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

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

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"
}