DocumentCode
3279461
Title
Efficient computation of a guaranteed stability domain for a high-order parameter dependent plant
Author
Roos, C. ; Biannic, J.
Author_Institution
Syst. Control & Flight Dynamics Dept., ONERA, Toulouse, France
fYear
2010
fDate
June 30 2010-July 2 2010
Firstpage
3895
Lastpage
3900
Abstract
A practical method based on μ-analysis is proposed in this paper to compute a robustness margin for high-order LTI plants with highly repeated parametric uncertainties. This margin is guaranteed on a continuous frequency interval and there is no risk of missing a critical frequency. The resulting algorithm is then encompassed in a recursive procedure, which computes a guaranteed stability domain for possibly uncertain parameter dependent plants. Several extensions and variations to handle the trade-off between conservatism and computational time are also highlighted. The efficiency of the method is finally demonstrated on a challenging industrial problem: assessing the stability of a flexible passenger aircraft over its entire flight envelope and for all admissible mass configurations.
Keywords
aircraft control; control system analysis; linear systems; stability; uncertain systems; μ-analysis; admissible mass configuration; continuous frequency interval; critical frequency; flexible passenger aircraft; flight envelope; guaranteed stability domain; high-order LTI plant; high-order parameter dependent plant; industrial problem; parametric uncertainty; recursive procedure; robustness margin; Aerospace industry; Constraint optimization; Frequency; Grid computing; High performance computing; Robust control; Robust stability; Robustness; Uncertainty; Upper bound;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2010
Conference_Location
Baltimore, MD
ISSN
0743-1619
Print_ISBN
978-1-4244-7426-4
Type
conf
DOI
10.1109/ACC.2010.5530661
Filename
5530661
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