摘要
建立了100N推力级微小型涡喷发动机模型,应用鲁棒控制算法进行了控制器软、硬件系统开发设计;提出了全新的仿真方法,用该方法对控制器进行了仿真,取得了良好的效果。电子控制器不仅具备等转速调节功能,且有足够的逻辑、多种控制监测和保护功能,完全符合多功能FADEC控制的要求。
A model for 100N class micro turbojet engine is established. Software and hardware system design of the controller is accomplished by using robust control algorithm. New simulation methods are applied to this controller and draw satisfactory results. This electronic controller has functions for not only constant rotation speed adjustment, but also functions of logic, multiple control monitoring and protection, which can meet the requirements of multifunctional FADEC control completely.
出处
《航空发动机》
2006年第1期38-42,共5页
Aeroengine
