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• W2773996957 abstract "Two approaches to tackle the nonlinear robust stability problem of an aerospace system are compared. The first employs a combination of the describing function method and μ analysis, while the second makes use of integral quadratic constraints (IQCs). The model analyzed consists of an open-loop wing's airfoil subject to free play and linear time-invariant parametric uncertainties. The key steps entailed by the application of the two methodologies and their main features are critically discussed. Emphasis is put on the available insight on the nonlinear postcritical behavior known as limit cycle oscillation. It is proposed a strategy to apply IQCs, typically used to find absolute stability certificates, in this scenario, based on a restricted sector bound condition for the nonlinearity. Another contribution of this paper is to understand how the conservatism usually associated with the IQCs multipliers selection can be overcome by using information coming from the first approach. Nonlinear time domain simulations showcase the prowess of these approaches in estimating qualitative trends and quantitative response's features." @default.
• W2773996957 created "2017-12-22" @default.
• W2773996957 creator A5044337546 @default.
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• W2773996957 date "2019-03-01" @default.
• W2773996957 modified "2023-10-17" @default.
• W2773996957 title "Nonlinear Robust Approaches to Study Stability and Postcritical Behavior of an Aeroelastic Plant" @default.
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• W2773996957 doi "https://doi.org/10.1109/tcst.2017.2779110" @default.
• W2773996957 hasPublicationYear "2019" @default.
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