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。
Aero engine accelerating control is one of researches of engine control.
发动机控制的重要研究内容。
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.
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。
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.
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。
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 this paper, the optimal PID control system for aero-engine was designed using LQR (Linear-Quadratic Regulator) approach.
本文采用基于LQR的PID控制算法，设计某型号涡扇发动机控制系统。
Research finding about the tip clearance of engine in the paper is basal; they can be used as reference of aero-engine design and the tip clearance control.
这些工作对于发动机初步设计设计和叶尖间隙控制理论研究有一定的参考价值。
Using time sequence method, the starting process of some aero-engine is controlled by starting control box.
某型发动机的起动过程采用时序控制方式，由起动程序机构来实行控制。
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。
A new neural network algorithm with fuzzy logic compensation was proposed and applied to an aero-engine rotating speed control system.
提出了一种带模糊补偿的神经网络辨识器，并应用在某型涡扇发动机转速控制系统中。
The research of reliable communication is always the key point on aero-engine distributed control system.
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。
Every module is built, tested and encapsulated into the aero-engine control system module library. Maked use of the module library, the engine system model can be established easily.
将模块封装打包建立涡扇发动机控制系统模型库，并将之组成为完整的发动机及调节器系统综合仿真平台。
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.
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。
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