DocumentCode
2088918
Title
Falsification of an aircraft autopilot
Author
Demourant, Fabrice ; Ferreres, Gilles ; Biannic, Jean-Marc
Author_Institution
Syst. Control & Flight Dynamics Dept., ONERA-CERT/DCSD, Toulouse, France
Volume
1
fYear
2002
fDate
2002
Firstpage
803
Abstract
The aim of this paper is to apply falsification techniques to the retuning of an aircraft autopilot, using experimental flight data. More precisely, an initial MIMO PI controller, synthesized with a modal technique on a simplified aircraft model, gives a poor performance on the real aircraft. Experimental flight data (generated in the context of our paper with a realistic complete auto-landing simulator) are used to directly retune this controller, without the intermediate step of building with these data a sophisticated nonlinear (possibly time-varying) aircraft model.
Keywords
MIMO systems; aircraft control; nonlinear systems; robust control; tuning; two-term control; MIMO system; PI controller; aircraft. control; autopilot; controller validation; experimental flight data; falsification techniques; nonlinear model; retuning; robust control; Aerospace control; Aerospace simulation; Aircraft manufacture; Buildings; Context modeling; Control systems; MIMO; Open loop systems; Robust control; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2002. Proceedings of the 2002
ISSN
0743-1619
Print_ISBN
0-7803-7298-0
Type
conf
DOI
10.1109/ACC.2002.1024913
Filename
1024913
Link To Document