Title of article
Gain Scheduling Control of Nonlinear Shock Motion Based on Equilibrium Manifold Linearization Model
Author/Authors
Tao، نويسنده , , Cui and Daren، نويسنده , , Yu and Wen، نويسنده , , Bao and Yongbin، نويسنده , , Yang، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2007
Pages
7
From page
481
To page
487
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.
Keywords
shock motion , equilibrium manifold linearization , gain scheduling control
Journal title
Chinese Journal of Aeronautics
Serial Year
2007
Journal title
Chinese Journal of Aeronautics
Record number
2264677
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