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航空发动机全包线最优PID控制器设计
引用本文:李述清,张胜修,刘毅男.航空发动机全包线最优PID控制器设计[J].弹箭与制导学报,2011,31(4):105-107.
作者姓名:李述清  张胜修  刘毅男
作者单位:第二炮兵工程学院,西安,710025
摘    要:研究了一种基于神经网络的航空发动机全包线PID控制器设计方法。首先在全包线内选定若干典型工况点,并通过遗传算法离线优化PID控制器参数。然后通过BP神经网络训练建立飞行高度和马赫数与PID参数的非线性映射关系,亦即建立起基于神经网络的航空发动机全包线最优PID控制器。最后,将该控制器应用于某型涡扇发动机稳态控制和飞行过程控制仿真,与原控制器比较,控制效果获得有效改善。

关 键 词:航空发动机  神经网络  PID控制  飞行包线

Neutral Network Based Optimal PID Controller over Whole Envelope for an Aero-engine
LI Shuqing,ZHANG Shengxiu,LIU Yinan.Neutral Network Based Optimal PID Controller over Whole Envelope for an Aero-engine[J].Journal of Projectiles Rockets Missiles and Guidance,2011,31(4):105-107.
Authors:LI Shuqing  ZHANG Shengxiu  LIU Yinan
Affiliation:LI Shuqing,ZHANG Shengxiu,LIU Yinan(The Second Artillery Engineering College,Xi'an 710025,China)
Abstract:An aero-engine optimal PID control scheme was presented,which was suitable for the engine whole envelope with a neural network approximation.Firstly,the optimal PID controller parameters were designed by genetic algorithm(GA) for a certain turbofan engine simplified real-time simulation model around some design-points.Then according to these optimized PID controller parameters,a neural network approximation was trained to imitate the relation between the parameters(Kp,Ki,Kd) of local optimal controllers and...
Keywords:turbofan engine  neutral network  PID control  flight envelope  
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