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基于卡尔曼滤波的航空发动机单神经元自适应控制
引用本文:王稳战,陈长发,胡金海.基于卡尔曼滤波的航空发动机单神经元自适应控制[J].燃气涡轮试验与研究,2012(1):40-43.
作者姓名:王稳战  陈长发  胡金海
作者单位:94106部队;空军工程大学工程学院
摘    要:针对航空发动机多任务、多变量、高精度和一体化控制的需求,提出了一种基于卡尔曼滤波的单神经元自适应控制方法。该方法在单神经元自适应控制算法的基础上,增加了对控制量和发动机反馈量的滤波,提高了响应速度,精度较高。仿真结果证明,该方法对过程噪声和测量噪声具有很强的克服能力,所需计算量较小,能满足发动机控制对实时性的要求。

关 键 词:航空发动机  卡尔曼滤波  单神经元  自适应控制  滤波  噪声

Single Neuron Adaptive Control System of Aero-Engine Based on Kalman Filter
WANG Wen-zhan,CHEN Chang-fa,HU Jin-hai.Single Neuron Adaptive Control System of Aero-Engine Based on Kalman Filter[J].Gas Turbine Experiment and Research,2012(1):40-43.
Authors:WANG Wen-zhan  CHEN Chang-fa  HU Jin-hai
Institution:1.Unit 94106,Xi’an 710614,China;2.Engineering Institute, Air Force Engineering University,Xi’an 710038,China)
Abstract:The single neuron adaptive control method based on Kalman filter is investigated to meet the demands of multi-mission,multi-variables and high precision of aero-engines.On the basis of single neuron adaptive control algorithm,the Kalman filter method enhances the filter on the control variables and feedback variables to over come the noises on the control performance.The simulation results indicated that the controller obtains satisfactory performance,which is effective inhibition of the filter to the process noise and measurement noise,is a useful tool for the sophisticated multi parameter system.
Keywords:aero-engine  Kalman filter  single neuron  adaptive control  filtering  noise
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