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

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

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Scopus citations

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.

Original languageEnglish
Title of host publicationICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006
PublisherInternational Council of The Aeronautical Sciences (ICAS)
Pages3205-3218
Number of pages14
ISBN (Print)9781604232271
StatePublished - 2006
Event25th Congress of the International Council of the Aeronautical Sciences 2006 - Hamburg, Germany
Duration: 3 Sep 20068 Sep 2006

Publication series

NameICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006
Volume5

Conference

Conference25th Congress of the International Council of the Aeronautical Sciences 2006
Country/TerritoryGermany
CityHamburg
Period3/09/068/09/06

Keywords

  • Flight control
  • Fly-by-wire
  • Transport aircraft

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