Detail výsledku

TECS/THCS Based Flight Control System for General Aviation

CHUDÝ, P.; RZUCIDŁO, P. TECS/THCS Based Flight Control System for General Aviation. 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. p. 1-13. ISBN: 978-1-56347-978-6.
Typ
článek ve sborníku konference
Jazyk
anglicky
Autoři
Chudý Peter, doc. Ing., Ph.D., MBA, UPGM (FIT)
Rzucidlo Pawel
Abstrakt

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

Klíčová slova

Flight Control, Control Laws, Aircraft

URL
Rok
2009
Strany
1–13
Sborník
Conference Proceeding Series (GNC/AFM/MST)
Řada
2009 AIAA Meeting Papers on Disc, Vol. 14, No. 9 (GNC/AFM/MST)
Konference
AIAA Modeling and Simulation Technologies Conference
ISBN
978-1-56347-978-6
Vydavatel
American Institute of Aeronautics and Astronautics
Místo
Chicago
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"
}
Projekty
Výzkum informačních technologií z hlediska bezpečnosti, MŠMT, Institucionální prostředky SR ČR (např. VZ, VC), MSM0021630528, zahájení: 2007-01-01, ukončení: 2013-12-31, řešení
Pracoviště
Ústav počítačové grafiky a multimédií (UPGM)
Nahoru