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Robust nonlinear stability and performance analysis of an F/A-18 aircraft model using sum of squares programming

Abstract:
In this paper, we develop algorithms for the computational analysis of stability and robust performance properties of nonlinear models governed by polynomial differential equations in quasi-Linear Parameter Varying form subject to parametric uncertainty. The methods presented use the sum of squares decomposition and ideas from real algebraic geometry to represent polynomial non-negativity over closed sets to compute various system properties such as L2 gain, regions of attraction, reachable sets and nonlinear Hankel norm approximations. The methods we present are then illustrated on a nonlinear model of an F/A-18 aircraft short-period dynamics subject to uncertainty in the aerodynamic coefficients. Copyright © 2012 John Wiley and Sons, Ltd.

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Publisher copy:
10.1002/rnc.2928

Authors

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Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author


Journal:
International Journal of Robust and Nonlinear Control More from this journal
Volume:
23
Issue:
10
Pages:
1099-1114
Publication date:
2013-07-10
DOI:
EISSN:
1099-1239
ISSN:
1049-8923


Language:
English
Keywords:
Pubs id:
pubs:404506
UUID:
uuid:eda188f9-6a65-4694-85c9-444649aafb62
Local pid:
pubs:404506
Source identifiers:
404506
Deposit date:
2013-11-17
ARK identifier:

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