New tools are presented for the computation of tight lower bounds on the st
ructured singular value mu for high-order plants subject to purely real par
ametric uncertainty. The first approach uses the mu-sensitivity function to
systematically reduce the order of the real uncertainty matrix, so that ex
ponential time lower bound algorithms can be applied. The second approach f
ormulates the search for a worst-case real destabilizing perturbation as a
constrained nonlinear optimization problem. Both approaches are applied to
the problem of analyzing the stability robustness properties of an integrat
ed flight and propulsion control system for an experimental vertical/short
takeoff and landing aircraft configuration. Currently available software to
ols for calculating lower bounds on real mu fail for this problem, whereas
both new approaches deliver tight bounds over the frequency range of intere
st.