• 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