Abstract
New tools are presented for the computation of tight lower bounds on the structured singular value μ, for high-order plants subject to purely real parametric uncertainty. The first approach uses the μ-sensitivity function to systematically reduce the order of the real uncertainty matrix, so that exponential time lower bound algorithms can be applied. The second approach formulates 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 integrated flight and propulsion control system for an experimental vertical/short takeoff and landing aircraft configuration. Currently available software tools for calculating lower bounds on real μ fail for this problem, whereas both new approaches deliver tight bounds over the frequency range of interest.
| Original language | English |
|---|---|
| Pages (from-to) | 1204-1213 |
| Number of pages | 10 |
| Journal | Journal of Guidance, Control, and Dynamics |
| Volume | 24 |
| Issue number | 6 |
| DOIs | |
| Publication status | Published - 2001 |