The paper introduces a new approach for the computation of a
lower bound on the structured singular value (SSV), μ in the
presence of purely real and mixed/complex uncertainties. The
approach utilises a frequency sweeping technique based on a
linear fractional transformation representation of structured uncertainty.
The technique is applied to a well-known civil transport
aircraft example. A fixed structure controller synthesis
strategy is developed, which addresses potential stability problems
that can occur using standard design methodologies.