舰船电子工程2019，Vol.39Issue(6)：94-97,4.DOI:10.3969/j.issn.1672-9730.2019.06.024
无人机发动机瞬态工况空燃比控制策略研究∗
Research on Air-Fuel Ratio Control Strategy of UAV Engine Transient Conditions
马攀伟 1贾强 1王栋 1贺根华 1柳鑫1
作者信息
摘要
Abstract
In order to solve the air-fuel ratio control problem of rotor engine of the UAV in transient conditions,based on the engine mean value model,combined with the actual working process of rotor engine,the intake system dynamic sub-model and fuel dynamic sub-model of rotor engine are established,and then utilized. The feedforward fuel dynamic compensator model is designed based on the inverse model principle,and the compensation effect is simulated and analyzed in Matlab/Simulink. The results show that the compensator model can effectively compensate the fuel injection amount in the transient condition of rotor engine,reduce the maximum deviation of the air-fuel ratio,and shorten the stable adjustment time of the air-fuel ratio.关键词
转子发动机/平均值模型/燃油动态补偿器/空燃比Key words
rotor engine/mean value model/fuel dynamic compensator/air-fuel ratio分类
交通工程引用本文复制引用
马攀伟,贾强,王栋,贺根华,柳鑫..无人机发动机瞬态工况空燃比控制策略研究∗[J].舰船电子工程,2019,39(6):94-97,4.
