Detail publikace

TECS/THCS Based Flight Control System for General Aviation

CHUDÝ, P. RZUCIDŁO, P.

Originální název

TECS/THCS Based Flight Control System for General Aviation

Typ

článek ve sborníku mimo WoS a Scopus

Jazyk

angličtina

Originální abstrakt

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.

Klíčová slova

Flight Control, Control Laws, Aircraft

Autoři

CHUDÝ, P.; RZUCIDŁO, P.

Rok RIV

2009

Vydáno

31. 8. 2009

Nakladatel

American Institute of Aeronautics and Astronautics

Místo

Chicago

ISBN

978-1-56347-978-6

Kniha

Conference Proceeding Series (GNC/AFM/MST)

Edice

2009 AIAA Meeting Papers on Disc, Vol. 14, No. 9 (GNC/AFM/MST)

Strany od

1

Strany do

13

Strany počet

13

URL

http://pdf.aiaa.org/preview/CDReadyMMST09_1999/PV2009_5689.pdf

BibTex

@inproceedings{BUT33794,
  author="Peter {Chudý} and Pawel {Rzucidlo}",
  title="TECS/THCS Based Flight Control System for General Aviation",
  booktitle="Conference Proceeding Series (GNC/AFM/MST)",
  year="2009",
  series="2009 AIAA Meeting Papers on Disc, Vol. 14, No. 9 (GNC/AFM/MST)",
  pages="1--13",
  publisher="American Institute of Aeronautics and Astronautics",
  address="Chicago",
  isbn="978-1-56347-978-6",
  url="http://pdf.aiaa.org/preview/CDReadyMMST09_1999/PV2009_5689.pdf"
}