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航空活塞式发动机瞬态空燃比控制仿真研究
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  • 英文篇名:Simulation research on transient air-fuel ratio control of aero piston engine
  • 作者:胡春明 ; 毕延飞 ; 王齐英 ; 仲伟军
  • 英文作者:HU Chunming;BI Yanfei;WANG Qiying;ZHONG Weijun;Tianjin Internal Combustion Engine Research Institute,Tianjin University;Stake Key Laboratory of Engines,Tianjin University;
  • 关键词:航空活塞式发动机 ; 过渡工况 ; 空燃比控制 ; 模型预测控制 ; 神经网络
  • 英文关键词:aero piston engine;;transition condition;;air-fuel ratio control;;model predictive control;;neural network
  • 中文刊名:HKDI
  • 英文刊名:Journal of Aerospace Power
  • 机构:天津大学天津内燃机研究所;天津大学内燃机燃烧学国家重点实验室;
  • 出版日期:2018-05-21 11:48
  • 出版单位:航空动力学报
  • 年:2018
  • 期:v.33
  • 基金:国家自然科学基金(51476112)
  • 语种:中文;
  • 页:HKDI201805026
  • 页数:9
  • CN:05
  • ISSN:11-2297/V
  • 分类号:221-229
摘要
针对航空活塞式直喷发动机瞬态空燃比难以精确控制、动态超调大等问题,采用基于改进的粒子群优化算法和Elman神经网络(VPSO-Elman网络)的模型预测控制算法对发动机过渡工况空燃比进行控制。在实验数据的基础上,利用发动机建模软件AMESim建立发动机模型,在MATLAB/Simulink中建立VPSO-Elman空燃比预测模型控制系统,通过联合仿真检验控制系统的性能。结果表明:瞬态工况下,相比于比例-积分-微分(PID)控制,VPSO-Elman网络模型预测控制下的空燃比超调量可以减小约20%,回调时间缩短约75%;针对不同的节气门开度变化速率,VPSO-Elman控制器同样具有良好的控制效果。
        In order to solve the problems like the large dynamic overshoot in the control of transient air-fuel ratio of aero piston engine,the model predictive control strategy based on improved particle swarm optimization algorithm and Elman(VPSO-Elman)neural network was proposed.The engine model used in the simulation was established based on a real engine in AMESim.The model predictive control system was established in MATLAB/Simulink.Coupling simulation was carried out to test the effect of the model prediction control.The simulation result shows that,compared with proportional integral derivative(PID)control,using VPSO-Elman network model prediction control the air-fuel overshoot can be reduced by 20%,callback time could be reduced by about 75%;for different throttle opening rate,VPSO-Elman controller also has a good control effect.
引文
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