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 language | English |
|---|---|
| Pages (from-to) | 481-487 |
| Number of pages | 7 |
| Journal | Chinese Journal of Aeronautics |
| Volume | 20 |
| Issue number | 6 |
| DOIs | |
| State | Published - Dec 2007 |
| Externally published | Yes |
Keywords
- Equilibrium manifold linearization
- Gain scheduling control
- Shock motion
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