Development of control laws for the simulation of a new transport aircraft

F. Holzapfel, O. da Costa, M. Heller, G. Sachs

Publikation: Beitrag in Buch/Bericht/KonferenzbandKonferenzbeitragBegutachtung

2 Zitate (Scopus)

Abstract

This paper presents the development of fly-bywire control laws used for the high-fidelity simulation of a new transport category aircraft. Beyond structural and gain design aspects for normal operations, also envelope protections and limitations as well as mode transition issues are addressed. As the control system is to be adjusted to changing aircraft datasets at different levels of fidelity, particular emphasis has been put on a high level of automation in gain design and system assessment routines.

OriginalspracheEnglisch
TitelICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006
Herausgeber (Verlag)International Council of The Aeronautical Sciences (ICAS)
Seiten3205-3218
Seitenumfang14
ISBN (Print)9781604232271
PublikationsstatusVeröffentlicht - 2006
Veranstaltung25th Congress of the International Council of the Aeronautical Sciences 2006 - Hamburg, Deutschland
Dauer: 3 Sept. 20068 Sept. 2006

Publikationsreihe

NameICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006
Band5

Konferenz

Konferenz25th Congress of the International Council of the Aeronautical Sciences 2006
Land/GebietDeutschland
OrtHamburg
Zeitraum3/09/068/09/06

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