并提出了增广l QL控制方法，应用其设计了航空发动机控制系统。
The augmented LQL method was proposed, then the aeroengine control system was designed by using the method.
航空发动机控制系统半物理模拟试验中，涡轮出口气体温度高、变化快，难以模拟。
In the matter - in - loop simulation experiment of aero - engine control system, the turbine outlet temperature, which characteristics with high and quick change , is hard to be simulated.
本文从数学模型和控制器两方面着手研究提高航空发动机控制系统自适应性的方法。
To improve the adaptive capability of aeroengine control system, the research on mathematic model and controller has been conducted in present thesis.
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