Adaptive inverse control structure for nonlinear systems is applied for aeroengine control systems.
研究了航空发动机的非线性自适应逆控制方案。
The augmented LQL method was proposed, then the aeroengine control system was designed by using the method.
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。
All experiments have showed that the design meets the requirements of distributed 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。
To improve the adaptive capability of aeroengine control system, the research on mathematic model and controller has been conducted in present thesis.
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。
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.
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 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 result indicates that the smart position actuator can be applied to aeroengine distributed control systems.
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 implies that this method has high precision and fast convergence pace and it can be applied to many fields such as aeroengine numeral simulation, control simulation and so on.
试验结果表明，此方法具有精度高，收敛速度快等优点，可广泛运用于发动机数值仿真及控制模拟等领域。
The optimal control of aeroengine acceleration and deceleration processes is deeply investigated.
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。
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.
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。
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 near deadbeat control design was applied to an aeroengine speed simulation system for flight handling simulation.
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。
In this paper, the theory and method of intelligence control are used to aeroengine multivariable control.
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。
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。
The fuel supply regulator was the major execution module of the comprehensive control system for an aeroengine.
供油调节器是航空发动机综合控制系统的主要执行机构。
This paper briefly introduces an application of dynamic data acquisition and processing system in an example with the pressure increasing limiter of a fuel control system of an aeroengine.
本文以某型航空发动机燃油调节系统的升压限制器为例，简要地介绍了一种动态数据采集与处理系统的应用。
An automatic control system of aeroengine test has been designed, based on the method of model reference adaptive control with restraints.
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。
A method of global sliding mode control was put forward for aeroengine with uncertainty and strong nonlinearity based on self-adaptive PSO neural network.
针对现代航空发动机是一个具有不确定性的强非线性系统，提出了一种基于自适应PSO网络整定的航空发动机全程滑模控制方法。
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.
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。
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。
This model has been applied to fault description of an aeroengine hydraulic mechanical control system, and...
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...
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。
应用推荐