Abstract
The influence of actuators on the dynamic performance of aeroengine control systems, and the intermediate state control systems design problem for certain model of aeroengine based on multivariable H∞ controller design theory was investigated. The comparative simulation results were provided on the platform of numerical simulation for control systems with and without actuators, which demonstrate that actuators can help controller constrain control energy and in the incremental direction of control signal, system considered possesses strong robust stability and performance.
| Original language | English |
|---|---|
| Pages (from-to) | 335-338 |
| Number of pages | 4 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 26 |
| Issue number | 4 |
| State | Published - Aug 2005 |
Keywords
- Aircraft engine
- Control system
- Numerical simulation
- Robust control
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