The proposed method can be applied to the establishment of the aeroengine state space model, which will be helpful in the multivariable digital electronic engine control system design.
这种方法为航空发动机多变量数字电子控制器的设计奠定了强有力的基础。
Engine tests of starting procedure control and rotation speed in closed loop have proven that the time precision and reliability of this software meet the demands of engine control system well.
在发动机台架上对微型涡喷发动机进行的起动过程控制和转速闭环调节试验表明，该控制软件在时间精度和可靠性方面能够满足发动机控制的要求。
The design and realization of a variable thrust liquid rocket engine control system is present in this paper.
本文讨论了某型变推力液体火箭发动机数字控制系统的设计和实现。
The measuring system of individual cell voltages is an important part of the fuel cell engine control system.
单片电压采集系统(CVM)是燃料电池发动机控制系统的重要组成部分之一。
A typical engine control system consists of three parts: sensors, electronic control unit (ECU) and executors.
典型的发动机控制系统由三部分组成：传感器、电控单元和执行器。
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 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。
According to Kalman filter and multiple-failure-hypothesis based testing, the sensor failures are detected, isolated and accommodated in turbofan engine control system.
研究利用卡尔曼滤波器及多重故障假设检验方法来检测某发动机控制系统传感器硬、软故障，并实现故障传感器的输出重构。
The simulations show that using the method not only can improve the dynamic performance of the engine control system, but also can guarantee the stability in some occasions.
仿真结果表明利用多回路切换控制方法在不影响系统安全性的前提条件下，可提高涡扇发动机的动态响应能力。
Moreover, the network construction was simple and normative, easy to be realized. The simulation result was satisfied for the aero-engine control system with broad working range.
而且该网络结构简单规范，便于实现，对于工作范围宽广的航空发动机控制系统，仿真效果令人满意。
This paper introduced the hardware and software constitution of the step-motor direct control system with PLC, and expounded the application in the engine control system in bench test.
介绍了运用PLC直接控制步进电机系统的软硬件组成，阐述了PLC直接控制步进电机技术在发动机台架试验测控系统中的应用。
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。
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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