1) concurrent control system
共行控制系统
2) shared control system
共享控制系统
1.
A Specific Database System Construction for Shared Control System;
共享控制系统的专用数据库设计方案
2.
Research on applying the extended state observer to model parameter identification for shared control systems
扩维观测器用于共享控制系统的模型参数辨识的研究
3.
Studies the construction of a model of networked control system,the Internet based shared control system.
研究基于因特网的共享控制系统这一全新的网络控制系统模型的构建方案。
3) GCS Global Control System
共用控制系统
4) operation control system
运行控制系统
1.
Research on Key Techniques of Centralized Operation Control System in Maglev Transportation System;
磁浮交通中央运行控制系统的关键技术研究
2.
Design of Maglev Operation Control System and Develop of Its Key Component;
磁浮列车运行控制系统设计及其核心部件研制
3.
The operation control system of Shanghai Maglev Demonstration Line plays a crucial role in the automatic control and safety protection of the train.
上海磁浮列车示范运行线的运行控制系统对列车运行起到自动控制和安全防护的核心作用。
5) travel control system
行程控制系统
6) flight control systems
飞行控制系统
1.
Wavelength Division Multiplexing(WDM) technology,one of the critical technologies of fly-by-light (FBL) flight control system, was studied in terms of the characteristics of flight control systems.
依据飞控系统的特点,研究了光传飞行控制系统关键技术之一的波分复用(WDM)多路传输技术,给出了可应用于飞控系统的波分复用多路光纤传输系统的具体实现方法,介绍了波分复用光电器件的选取,硬件电路的设计方法,并从工程应用角度出发,将其应用于舰载飞机着舰的可视化仿真平台中,仿真结果显示该系统具有良好的性能,为波分复用技术在光传飞控系统中的进一步应用研究提供了基础。
2.
The designing approach of nonlinear robust dynamic inversion for flight control systems is discussed, and a new control strategy with robust stability is presented, which will be needed to account for uncertain effects related with unknown parameters and external disturbance while in supermaneuver flight, and a stability result is got about this control strategy in case of parameters perturbation.
对非线性飞行控制系统的非线性鲁棒动态逆设计方法作了研究，给出了一种具有鲁棒稳定的非线性动态逆控制方案，以克服飞机在机动飞行时，被控对象参数不确定性和外干扰对系统稳定性的影响，并给出了该方案在这种情况下的稳定性结果。
3.
The eigenstructure assignment method is an efficient approach in designing multi-mode flight control systems ,which could determine the expected control law directly through integrating the system performance index with the flight quality requirements of aircraft.
特征结构配置法是设计多模态飞行控制系统一种较为有效的方法。
补充资料：反馈控制(见控制系统)
反馈控制(见控制系统)
feedback control
于。。伙。]伙ongZ片}反馈控制(几edbaekcontrol)见拉制系统。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条