Skip to main navigation Skip to search Skip to main content

Design of self-scheduled H control for turbofan engine

  • Yan Feng Sui*
  • , Da Ren Yu
  • , Peng Sui
  • *Corresponding author for this work
  • School of Energy Science and Engineering, Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

The LPV (Linear Parameter-Varying) system of turbofan engine was put into a polytopic expression by a convex decomposition, and the polytopic features were used to simplify the controller design to a vertices' controller design. By using a LMI (Linear Matrix Inequality) approach, a feedback controller with the pole placement in a given region and with unique Lyapunov function for every vertex was designed, which satisfied H performance requirement. A global continuous gain scheduled controller was then obtained by the synthesis of the vertex controllers. As compared with PID controller, the designed controller demonstrates its feasibility.

Original languageEnglish
Pages (from-to)857-861
Number of pages5
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume20
Issue number5
StatePublished - Oct 2005
Externally publishedYes

Keywords

  • Aerospace propulsion system
  • Gain scheduling
  • H control
  • Output feedback
  • Pole placemen
  • Polytope
  • Turbofan engine

Fingerprint

Dive into the research topics of 'Design of self-scheduled H control for turbofan engine'. Together they form a unique fingerprint.

Cite this