并提出了增广lQL控制方法，应用其设计了航空发动机控制系统。
The augmented LQL method was proposed, then the aeroengine control system was designed by using the method.
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.
本文从数学模型和控制器两方面着手研究提高航空发动机控制系统自适应性的方法。
To improve the adaptive capability of aeroengine control system, the research on mathematic model and controller has been conducted in present thesis.
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。
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.
基于基本模糊控制存在的问题，通过引入改进的模糊控制方法，基本满足了航空发动机控制系统的性能要求。
In view of the existing problem of general fuzzy control, by introducing the improved fuzzy control, it has met the performance need of the aero-engine basically.
本文介绍了在航空发动机闭环控制系统的反馈通路上施加伪随机试验信号时，对发动机模型参数进行辨识的方法。
An aeroengine model can be identified from actual closed-loop engine test data if pseudorandom binary sequence as test signal ACTS on feedback circuit of the closed-loop control system.
供油调节器是航空发动机综合控制系统的主要执行机构。
The fuel supply regulator was the major execution module of the comprehensive control system for an aeroengine.
提出了航空发动机防喘控制系统设计和研制方法，分析了当战斗机发射导弹时热扰动参数对发动机的影响。
The design and development methods of aeroengine anti-surge control system are presented. Effects of heat disturbance parameters on the engine are analyzed during missile launch.
将模型应用于航空发动机液压机械控制系统的描述，并自动建造故障树，取得了较好的效果。
This model has been applied to fault description of an aeroengine hydraulic mechanical control system, and the fault tree has been built automatically, in result a success has been reached.
采用全权限数字式电子控制技术是航空发动机控制的一种发展趋势，电子控制器是控制系统中最核心的部分。
The technology of full authority digital electronic control is a trend of aeroengine control, and the electronic controller is the primary part in an aeroengine control system.
实验表明设计的通信方案可以满足航空发动机分布式控制系统要求。
All experiments have showed that the design meets the requirements of distributed aeroengine control system.
对采用模型参考自适应控制方法设计带有多项约束条件的航空发动机试车自动试车控制系统进行了研究。
An automatic control system of aeroengine test has been designed, based on the method of model reference adaptive control with restraints.
实验结果表明该智能位置控制器适用于航空发动机分布式控制系统。
The result indicates that the smart position actuator can be applied to aeroengine distributed control systems.
将模型应用于航空发动机液压机械控制系统的描述，并自动建造故障树，取得了较好的效果。
This model has been applied to fault description of an aeroengine hydraulic mechanical control system, and...
本文详细讨论了航空发动机滑油系统试验台计算机控制系统的软、硬件设计的过程和方法。
In this paper, the design of both the software and the hardware of the computer control system for the test-bed of lubricating oil system for aeroengine are discussed explicitly.
通讯的可靠性研究一直是航空发动机分布式控制系统研究的关键问题。
The research of reliable communication is always the key point on aero-engine distributed control system.
航空发动机采用分布式控制系统能大大降低发动机总体重量；
The application of the ADCS can greatly reduce the weight of the control system;
仿真研究了该控制算法和控制器的特性，结果表明用该控制方法设计的航空发动机模糊控制系统获得了满意的控制性能。
The research focuses on the algorithms and the property of this controller, as well as its application in aeroengine control by computer simulation. The results show that this method is...
仿真研究了该控制算法和控制器的特性，结果表明用该控制方法设计的航空发动机模糊控制系统获得了满意的控制性能。
The research focuses on the algorithms and the property of this controller, as well as its application in aeroengine control by computer simulation. The results show that this method is...
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