Abstract
This paper investigates the effectiveness of the structured singular value, μ, as a tool for analysing the stability robustness of an integrated flight and propulsion control (IFPC) system for an experimental STOVL aircraft configuration. Solutions of the resulting μ analysis problem reveal the somewhat conservative results provided by current software for computing μ with strictly real parameter uncertainty.
Original language | English |
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Pages (from-to) | 4529-4530 |
Number of pages | 2 |
Journal | Proceedings of the IEEE Conference on Decision and Control |
Volume | 5 |
Publication status | Published - 1999 |
Event | The 38th IEEE Conference on Decision and Control (CDC) - Phoenix, AZ, USA Duration: 7 Dec 1999 → 10 Dec 1999 |