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 language | English |
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Title of host publication | ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006 |
Publisher | International Council of The Aeronautical Sciences (ICAS) |
Pages | 3205-3218 |
Number of pages | 14 |
ISBN (Print) | 9781604232271 |
State | Published - 2006 |
Event | 25th Congress of the International Council of the Aeronautical Sciences 2006 - Hamburg, Germany Duration: 3 Sep 2006 → 8 Sep 2006 |
Publication series
Name | ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006 |
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Volume | 5 |
Conference
Conference | 25th Congress of the International Council of the Aeronautical Sciences 2006 |
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Country/Territory | Germany |
City | Hamburg |
Period | 3/09/06 → 8/09/06 |
Keywords
- Flight control
- Fly-by-wire
- Transport aircraft