An Aeroengine Adaptive Inverse Control Method Based on U-Model

摘要

This paper applies the U-model control method, combined with the traditional adaptive inverse control method, to the aeroengine speed control design, directly obtaining the engine fuel flow through the inverse controller. The proposed method does not need the complex engine model, and greatly simplifies the complex conventional controller design process. The simulation results show that the U-model-based adaptive inverse controller has an acceptable engine speed control performance in small and large transient responses.