QFT control of aeroengine through LMI-based diagonal dominance pre-compensation

Hua Cong Li, Xiao Bao Han, Zhi Kun Wu

科研成果: 期刊稿件文章同行评审

1 引用 (Scopus)

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
22
9
出版状态已出版 - 9月 2007

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