Designer in Aero-Engine Control System 控制系统总体设计员
Aero-Engine Control System Integration Position 控制系统总体集成岗 ; 沈阳
aero-engine control system 航空发动机控制系统
Aero-Engine Control System Integration Po 控制系统总体集成岗
aero-engine control unit 航空发动机控制器
Model of Aero-Engine Control System 发动机控制器模型
Aero-Engine Control System Design Position 沈阳
aero-engine transient control 航空发动机过渡态控制
aero-engine steady state control 航空发动机稳态控制
In this paper, a new variable structure control method, that is, Global variable structure control (GVSC), is introduced to aero engine control system.
针对直接驱动的交流永磁直线伺服系统，提出一种基于神经元补偿控制的全程滑模变结构控制策略。
A new neural network adaptive control scheme is presented and its applications to aero-engine control system are researched.
本文研究神经网络自适应控制方法及其在航空发动机控制中应用。
In the matter - in - loop simulation experiment of aero - engine control system, the turbine outlet temperature, which characteristics with high and quick change , is hard to be simulated.
航空发动机控制系统半物理模拟试验中，涡轮出口气体温度高、变化快，难以模拟。
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