摘要
Based on linear matrix inequalities (LMI) and quantitative feedback theory (QFT), a new design method of aeroengine robust controller was developed for uncertain mathematical model of aeroengine. The method has combined the design problem of frequency domain diagonal dominance pre-compensator and the solving process of LMI, thus achieving the decoupling of uncertain control objects. Moreover, a robust controller was designed with induction of QFT. The simulation results show that this method has good control efficiency and engineering applicability.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 1583-1587 |
| 页数 | 5 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 22 |
| 期 | 9 |
| 出版状态 | 已出版 - 9月 2007 |