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Gain scheduling control of nonlinear shock motion based on equilibrium manifold linearization model

  • Tao Cui*
  • , Daren Yu
  • , Wen Bao
  • , Yongbin Yang
  • *Corresponding author for this work
  • School of Energy Science and Engineering, Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

The equilibrium manifold linearization model of nonlinear shock motion is of higher accuracy and lower complexity over other models such as the small perturbation model and the piecewise-linear model. This paper analyzes the physical significance of the equilibrium manifold linearization model, and the self-feedback mechanism of shock motion is revealed. This helps to describe the stability and dynamics of shock motion. Based on the model, the paper puts forwards a gain scheduling control method for nonlinear shock motion. Simulation has shown the validity of the control scheme.

Original languageEnglish
Pages (from-to)481-487
Number of pages7
JournalChinese Journal of Aeronautics
Volume20
Issue number6
DOIs
StatePublished - Dec 2007
Externally publishedYes

Keywords

  • Equilibrium manifold linearization
  • Gain scheduling control
  • Shock motion

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