Research On Aeroengine Neural Network Inverse Control Method

摘要：

　　A certain type biaxial turbofan aeroengine component level Nonlinear systems as research subjects, by using neural network inverse control method is the study of aviation engine identification based on improved particle swarm optimization BP network, by increasing the feedback link, improve the control precision inverse control system,inverse control system has to eliminate static error.At the same time select the sample values for different operating points within the flight envelope aeroengine research, control performance to verify the designed aeroengine neural network inverse control system.

关键词： Aircraft engine Neural network inverse control Improved particle swarm Optimization

作者: Ying Jin Huang Fangting Dai Jiyang

作者单位: Nanchang Hangkong University, Nanchang 330063, China;Nondestructive Test Key Laboratory of Ministry Education, Nanchang Hangkong University,Nanchang 330063, China

会议类型: 国际会议

会议名称: International Conference on Computational Science and Engineering Applications(CSEA2015)2015计算机科学与工程应用国际会议

会议地点: 三亚

会议语种:英文

页码: 518-523

在线出版日期: 2015-12-26（万方平台首次上网日期，不代表论文的发表时间）