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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&#39;s airfoil subject to free play and linear time-invariant parametric uncertainties. The key steps en...

Nonlinear Robust Approaches to Study Stability and Postcritical Behavior of an Aeroelastic Plant