DocumentCode :
3113922
Title :
Nonlinear Robust Performance Analysis using Gradient-Based Optimisation - An Aeroelastic Case-Study
Author :
Kim, Jongrae ; Bates, Declan G. ; Postlethwaite, Ian
Author_Institution :
Department of Engineering, University of Leicester, Leicester, LE1 7RH, United Kingdom jrk7@le.ac.uk
fYear :
2005
fDate :
12-15 Dec. 2005
Firstpage :
2781
Lastpage :
2786
Abstract :
This paper considers the problem of computing lower bounds on the worst-case performance of nonlinear systems using gradient-based optimisation. Four different gradient-based local optimisation methods are applied to a robust performance analysis problem for a nonlinear aeroelastic system. The first method formulates the optimisation problem in the classical Euler-Lagrange setting and computes the gradient by backward integration of the resulting adjoint system. The second method also uses the Euler-Lagrange formulation, but uses complex perturbations to calculate the gradient. The third method employs Sequential Quadratic Programming, while the fourth method considered is Simultaneous Perturbation Stochastic Approximation (SPSA), which uses a stochastic approach to decide the search direction. The performance of all four methods is evaluated in terms of computational complexity, numerical accuracy, and ease of implementation, and compared with a standard industrial approach based on a gridding of the uncertain parameter space.
Keywords :
Aerospace industry; Computational complexity; Computer industry; Nonlinear systems; Optimization methods; Performance analysis; Quadratic programming; Robust stability; Robustness; Stochastic processes;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2005 and 2005 European Control Conference. CDC-ECC '05. 44th IEEE Conference on
Print_ISBN :
0-7803-9567-0
Type :
conf
DOI :
10.1109/CDC.2005.1582584
Filename :
1582584
Link To Document :
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