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。
A new neural network adaptive control scheme is presented and its applications to aero-engine control system are researched.
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.
本文提出一种新的变结构自适应控制方法，并将其应用于航空发动机控制。
A new variable structure adaptive control scheme is proposed. The scheme consists of conventional model reference adaptive control and sliding mode control.
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.
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.
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.
航空发动机参数测试系统是由VFP系统总控软件来控制。
It is VFP system control software which controls the parameters measurement system of airplane engine.
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.
本文研究了飞行训练用航空发动机转速模拟系统拟最少拍控制设计。
The near deadbeat control design was applied to an aeroengine speed simulation system for flight handling simulation.
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.
对于像航空发动机这样复杂的非线性系统，基于对象精确数学模型的PID控制方法的自适应性较差，难以适应具有非线性、时变不确定性的被控对象。
Complicated nonlinear systems such as aircraft engines. PID control method which is based on precise mathematical model has poor adaptability and is not adaptive to nonlinear and time-variant plants.
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.
提出了一种基于航空发动机约束物理意义的寻优方法，并将其应用于性能寻优控制之中。
Presented a new method based on the physical characteristic of aero-engine constraint for performance seeking control, which consists of active set method and generalized reduced gradient method.
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.
提出了民用航空发动机空中停车率与维修成本控制的优化决策方法。
Optimization methods to control the in flight shutdown rate and the maintenance cost of civil aero engines are presented in this paper.
本文将智能控制理论和方法引入到航空发动机多变量控制中。
In this paper, the theory and method of intelligence control are used to aeroengine multivariable control.
本文阐述一个可用于航空发动机数据检测和控制的光纤传输系统。
This paper deals with a optical fiber transmisson system being used for detecting and control of aeroengines.
简要介绍了对某型航空发动机在外场使用过程中，实施战斗与训练状态控制的方法及其相应的控制装置。
The fight and train state control method as well as the control device for the engine in airport using is briefly introduced.
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.
深入研究了航空发动机加速过程和减速过程的最优控制问题。
The optimal control of aeroengine acceleration and deceleration processes is deeply investigated.
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.
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.
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...
因此，本文研究设计了一种使用于航空发动机篦齿间隙测量的基于PMAC自动控制卡的精密测量系统。
This paper studies an accurate measuring system based on PMAC motion controller's structure, which can be used to measuring the clearance of labyrinth.
作者认为，对于航空发动机这种严重非线性被控对象，选择合适的神经网络控制方案有着明显的优势。
The author believes that adopting appropriate control strategy based on neural network in aero-engine control has obvious advantage.
作者认为，对于航空发动机这种严重非线性被控对象，选择合适的神经网络控制方案有着明显的优势。
The author believes that adopting appropriate control strategy based on neural network in aero-engine control has obvious advantage.
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