Abstract
This paper considers the problem of reference tracking control for the flexible air-breathing hypersonic flight vehicle with actuator delay and uncertainty. By constructing the Lyapunov functional including the lower and upper bounds of the time-varying delay, the non-fragile controller is designed such that the resulting closed-loop system is asymptotically stable and satisfies a prescribed performance cost index. The simulation results are given to show the effectiveness of the proposed control method, which is validated by excellent output reference altitude and velocity tracking performance.
| Original language | English |
|---|---|
| Pages (from-to) | 141-145 |
| Number of pages | 5 |
| Journal | Journal of Systems Engineering and Electronics |
| Volume | 22 |
| Issue number | 1 |
| DOIs | |
| State | Published - Feb 2011 |
Keywords
- Actuator delay
- Flexible air-breathing hypersonic flight vehicle (FAHFV)
- Non-fragile control
- Output tracking control
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