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Output Feedback Control of Surge and Rotating Stall in Axial Compressors

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Publication:5270461
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DOI10.1002/ASJC.1384zbMath1365.93192OpenAlexW2524468327MaRDI QIDQ5270461

Wei Huang, Hanlin Sheng, Tianhong Zhang

Publication date: 23 June 2017

Published in: Asian Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/asjc.1384


zbMATH Keywords

active controloutput feedbacksurgeaero-enginerotating stallaxial compressor


Mathematics Subject Classification ID

Feedback control (93B52) Application models in control theory (93C95) Control/observation systems governed by ordinary differential equations (93C15)


Related Items (1)

A numerical strategy for modelling rotating stall in core compressors




Cites Work

  • High-gain feedback control of rotating stall in axial flow compressors
  • Nonlinear control of surge in axial compression systems
  • Active control of compressor stall inception: A bifurcation-theoretic approach
  • A survey of applications of second-order sliding mode control to mechanical systems




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