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.

• 针对航空发动机数学模型的不确定性，提出一种基于线性矩阵不等式(LMI)和定量反馈理论(QFT)的航空发动机鲁棒控制器的新的设计方法。