DocumentCode
2085822
Title
Online nonlinear guaranteed estimation with application to a high performance aircraft
Author
Scholte, Eelco ; Campbell, Mark E.
Author_Institution
Depaxtment of Mech. & Aerosp. Eng., Cornell Univ., Ithaca, NY, USA
Volume
1
fYear
2002
fDate
2002
Firstpage
184
Abstract
The most commonly used filters (or estimators) for online control customization are based upon stochastic assumptions on the noise. In this paper a set-membership filter is extended to be used with nonlinear systems for which the Jacobian and Hessian are continuous over the uncertainty interval. This filter relies on assuming that the noise sources are bounded in order to obtain hard bounds on state and parameter estimates. These bounds are then compatible with robust control design so that the controller can be adequately updated in real-time. The method proposed is referred to as an extended set-membership filter and is applied to a two-state example and to the state and parameter estimations of a complex F-15 like model.
Keywords
aircraft control; military aircraft; nonlinear systems; parameter estimation; real-time systems; robust control; state estimation; high performance aircraft; military aircraft; nonlinear guaranteed estimation; nonlinear systems; parameter estimation; real time control; robust control; set-membership filter; state estimation; Aerospace control; Aircraft propulsion; Filters; Missiles; Nonlinear systems; Parameter estimation; Robust control; State estimation; Stochastic resonance; Uncertainty;
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.2002.1024801
Filename
1024801
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