Abstract
A two-tier architecture of hierarchical control is proposed for future generation rotorcraft that demand enhanced performance and reliability. The continuously-varying controller at the lower tier is designed using probabilistic robust control approaches. The discrete-event supervisory controller at the upper tier is built upon the concepts of time-frequency analysis, symbolic dynamics, and automata theory. Results of simulation experiments based on the GENHEL model of UH-60 Black Hawk helicopter are presented.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 1707-1712 |
| Number of pages | 6 |
| Journal | Proceedings of the American Control Conference |
| Volume | 2 |
| State | Published - 2004 |
| Event | Proceedings of the 2004 American Control Conference (AAC) - Boston, MA, United States Duration: Jun 30 2004 → Jul 2 2004 |
All Science Journal Classification (ASJC) codes
- Electrical and Electronic Engineering