Publication detail

TECS/THCS Based Flight Control System for General Aviation

CHUDÝ, P. RZUCIDŁO, P.

Original Title

TECS/THCS Based Flight Control System for General Aviation

Type

article in a collection out of WoS and Scopus

Language

English

Original 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.

Keywords

Flight Control, Control Laws, Aircraft

Authors

CHUDÝ, P.; RZUCIDŁO, P.

RIV year

2009

Released

31. 8. 2009

Publisher

American Institute of Aeronautics and Astronautics

Location

Chicago

ISBN

978-1-56347-978-6

Book

Conference Proceeding Series (GNC/AFM/MST)

Edition

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

Pages from

1

Pages to

13

Pages count

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"
}