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
Anglický název
TECS/THCS Based Flight Control System for General Aviation
Jazyk
en
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.
Anglický 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.
Dokumenty
BibTex
@inproceedings{BUT33794,
author="Peter {Chudý} and Pawel {Rzucidlo}",
title="TECS/THCS Based Flight Control System for General Aviation",
annote="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.",
address="American Institute of Aeronautics and Astronautics",
booktitle="Conference Proceeding Series (GNC/AFM/MST)",
chapter="33794",
edition="2009 AIAA Meeting Papers on Disc, Vol. 14, No. 9 (GNC/AFM/MST)",
howpublished="print",
institution="American Institute of Aeronautics and Astronautics",
year="2009",
month="august",
pages="1--13",
publisher="American Institute of Aeronautics and Astronautics",
type="conference paper"
}