Abstract
In this effort system parameters are adaptively varied to identify bifurcations from equilibrium in simulations of a reduced-order model for turbomachinery aeromechanics. An element of the adaptive process is identification of a low-order locally nonlinear discrete-time map from the observables. The nonlinear behavior of the system in the neighborhood of the bifurcation is then estimated from the identified system.
| Original language | English (US) |
|---|---|
| Pages | 1146-1150 |
| Number of pages | 5 |
| State | Published - 1999 |
| Event | Proceedings of the 1999 IEEE International Conference on Control Applications (CCA) and IEEE International Symposium on Computer Aided Control System Design (CACSD) - Kohala Coast, HI, USA Duration: Aug 22 1999 → Aug 27 1999 |
Other
| Other | Proceedings of the 1999 IEEE International Conference on Control Applications (CCA) and IEEE International Symposium on Computer Aided Control System Design (CACSD) |
|---|---|
| City | Kohala Coast, HI, USA |
| Period | 8/22/99 → 8/27/99 |
All Science Journal Classification (ASJC) codes
- Control and Systems Engineering
Fingerprint
Dive into the research topics of 'Adaptive detection of instabilities and nonlinear analysis of a reduced-order model for flutter and rotating stall in turbomachinery'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver