Bifurcation Based Nonlinear Feedback Control for Rotating Stall in Axial Compressors,
Abstract
Classical bifurcation analysis for nonlinear dynamics is used to derive a nonlinear feedback control law that eliminates the hysteresis loop associated with rotating stall and extends the stable operating range in axial compressors. The proposed control system employs pressure rise as output measurement and throttle position as actuating signal for which both sensor and actuator exist in the current configuration of axial compressors. Thus our results provide a practical solution for rotating stall control in axial compressors.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1996
- Accession Number
- ADA320346
Entities
People
- Andrew Sparks
- Guoxiang Gu
- Siva Banda
Organizations
- Wright Laboratory