全状态

• In the paper , useful attempts and research on adaptive control are developed for a turbofan engine . a model reference adaptive control ( mrac ) using input and output measurements and pi adaptive law are applied to aeroengine multi - variable control system . simulation results show that controller avoids the measurement of full states variables and has good control performance
  将利用输入输出测量值的模型参考自适应控制方法和比例?积分型自适应律应用于航空发动机多变量控制中，并进行了数字仿真研究，结果表明控制器有效地避免了全状态量的测量，并获得好的动、静态性能。