The effectiveness of aero control decreases as dynamic pressure decreases. Therefore impulse attitude control motor(ACM) is to be used to maintain fast response of missile in low dynamic pressure.
气动控制在低动压时其效率会有相当下降，为了使导弹在低动压时仍然具有一定的快速响应性，在导弹上安装脉冲姿控发动机参与姿态控制是一条可行的途径。
The improvement of fire control system is an important method to heighten the efficiency of aero-weapons system.
航空火力控制系统的改进是提升飞机武器系统作战效能的一个重要手段。
Optimization methods to control the in flight shutdown rate and the maintenance cost of civil aero engines are presented in this paper.
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。
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。
Since the aero maintenance cost takes a very great portion of the total operation cost of airlines, it is important to control the maintenance cost effectively for total cost control.
航空维修成本在航空企业总成本中占据非常大的比例，有效控制维修成本对航空公司控制总成本具有重要作用。
The control moment from control law is allocated to aero-surface and reaction control system, in this phase the limits from hardware are taken into consideration.
将控制律给出的控制力矩合理分配给气动面的反作用控制系统，并考虑了实际的硬件特性要求。
The features of the BTT control method determine that its mathematical model contains many coupling elements, such as kinematical coupling, aero dynamical coupling, inertial coupling etc.
BTT飞行的特点决定了控制系统存在着运动学耦合、气动耦合和惯性耦合等多种耦合因素。
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。
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。
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。
Discussing a kind of power topological solution and its current control method of the three-phase energy feedback type electronic power load used in aero-generator testing.
论述了一种用于航空发电机测试用的三相馈能式电子负载功率拓扑方案及其电流控制策略。
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。
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 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。
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。
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。
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。
GZK series Aero-Obstruction Lantern Control Box is the corollary equipment of CZ series Aero-Obstruction Lantern.
GZK系列智能型航空障碍灯集中控制箱，是GZ系列航空障碍灯的配套产品。
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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