Detail publikace

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

CHUDÝ, P. RZUCIDŁO, P.

Originální název

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

Typ

článek ve sborníku mimo WoS a Scopus

Jazyk

angličtina

Originální abstrakt

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.

Klíčová slova

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

Autoři

CHUDÝ, P.; RZUCIDŁO, P.

Rok RIV

2010

Vydáno

26. 7. 2010

Nakladatel

Rzesow University of Technology

Místo

Bezmiechowa

ISBN

978-83-7199-623-8

Kniha

Conference of Avionics

Strany od

1

Strany do

8

Strany počet

8

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"
}