新的参考模型自适应控制方法在航空发动机中的应用
A New Model Reference Adaptive Control for Aeroengine
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摘要: 本文针对航空发动机模型的结构和参数不能明确已知,提出一种阶次低、鲁棒性较好的参考模型自适应控制法,即只需知道系统的相对阶次,且控制器结构简单,易于实现,适应性强。Abstract: A new model reference adaptive control method with excellent robustness is proposed for aeroengine.This method only needs to know the relative degree of the system.Its controller structure is simple and can be realized easily.Simulation results show that this controller can make system track the model reference output quite well.It has high adaptivity to the change of aeroengine model parameters and structure.
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Key words:
- aeroengine /
- model reference adaptive control /
- robustness
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