以工程应用为目的,采用输入输出模型参考自适应控制方法设计了航空发动机转速模型参考自适应控制器(Model reference adaptive control,MRAC)。针对发动机的非线性特性,设计了函数连接型神经网络补偿器。开展了控制器实物在回路仿真试验,结果表明基于非线性补偿的MRAC在包线内具有良好的动静态性能,对于发动机及其工作环境的非线性具有良好的补偿能力和适应性,验证了自适应控制方法在航空发动机工程应用中的有效性。 For engineering purposes, a model reference adaptive control (MRAC) model of aeroengine is designed by using I / O model reference adaptive control method. For the nonlinear characteristics of the engine, a function-connected neural network compensator is designed. The simulation results show that the MRAC based on nonlinear compensation has good static and dynamic performance in the covered wire and has good compensation ability and adaptability to the nonlinearity of the engine and its working environment. Effectiveness of Adaptive Control Method in Aeroengine Engineering Application.