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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
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" }