Publication Details

TECS/THCS Based Flight Control System for General Aviation

CHUDÝ Peter and RZUCIDŁO Paweł. TECS/THCS Based Flight Control System for General Aviation. In: Conference Proceeding Series (GNC/AFM/MST). 2009 AIAA Meeting Papers on Disc, Vol. 14, No. 9 (GNC/AFM/MST). Chicago: American Institute of Aeronautics and Astronautics, 2009, pp. 1-13. ISBN 978-1-56347-978-6.
Czech title
TECS/THCS systém řízení letu pro všeobecné letectví
Type
conference paper
Language
english
Authors
Chudý Peter, doc. Ing., Ph.D. MBA (DCGM FIT BUT)
Rzucidło Paweł, Ph.D. Eng. (RUT)
URL
Keywords

Flight Control, Control Laws, Aircraft

Abstract

The advantage of the TECS over classical control law designs proved to be in excellent performance and moderate complexity of the resulting controller structure. TECS/THCS's expected ability to support proven analytical tools compatible with the airworthiness certification procedure makes it an ideal candidate for implementation on board of a General Aviation aircraft.

Annotation

This paper discusses the implementation of TECS and THCS based flight controller for a low-end general aviation application. TECS is based on energy distribution logic, whereas THCS uses lateral/directional criteria for aircraft control. TECS/THCS control system was subjected to simulations.

Published
2009
Pages
1-13
Proceedings
Conference Proceeding Series (GNC/AFM/MST)
Series
2009 AIAA Meeting Papers on Disc, Vol. 14, No. 9 (GNC/AFM/MST)
Conference
AIAA Modeling and Simulation Technologies Conference, Hyatt Regency McCormick Place Chicago, Illinois, US
ISBN
978-1-56347-978-6
Publisher
American Institute of Aeronautics and Astronautics
Place
Chicago, US
BibTeX 
@INPROCEEDINGS{FITPUB9011,
   author = "Peter Chud\'{y} and Pawe\l Rzucid\lo",
   title = "TECS/THCS Based Flight Control System for General Aviation",
   pages = "1--13",
   booktitle = "Conference Proceeding Series (GNC/AFM/MST)",
   series = "2009 AIAA Meeting Papers on Disc, Vol. 14, No. 9 (GNC/AFM/MST)",
   year = 2009,
   location = "Chicago, US",
   publisher = "American Institute of Aeronautics and Astronautics",
   ISBN = "978-1-56347-978-6",
   language = "english",
   url = "https://www.fit.vut.cz/research/publication/9011"
}
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