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 language | English |
|---|---|
| Pages (from-to) | 857-861 |
| Number of pages | 5 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 20 |
| Issue number | 5 |
| State | Published - Oct 2005 |
| Externally published | Yes |
Keywords
- Aerospace propulsion system
- Gain scheduling
- H control
- Output feedback
- Pole placemen
- Polytope
- Turbofan engine
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