1) Flying Shear Control System
飞剪控制系统
1.
Study on the Hot-Roll-Line Flying Shear Control System;
热轧生产线飞剪控制系统的设计与实现
3) auto-control system for flying shears
剪自动控制系统
1.
Principle and operation of the auto-control system for flying shears;
飞剪自动控制系统的工作过程和原理
5) 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。
6) FCS
飞行控制系统
1.
How to select the object function parameter of the niche genetic algorithm(NGA) and its initial swarm is a very difficult problem when the NGA is applied in the optimization of flight control systems(FCS).
将小生境遗传算法(NGA)应用于飞行控制系统(FCS)的优化设计中,需要解决两个问题:如何选择目标函数及如何确定初始种群和算法运行参数。
2.
To optimize the parameters of the aircraft s flight control system(FCS),a reference model method based on the niche genetic algorithm(NGA)is proposed in this paper.
针对飞行控制系统控制器参数优化问题,提出了一种基于小生境遗传算法的模型参考优化整定策略,并将此策略应用于某型飞机的横侧向飞行控制系统的参数优化中。
3.
It is shown that the method can tune the parameters of the FCS,and converge faster,simply programmed.
针对飞行控制系统控制器参数优化问题,文中提出了一种基于粒子群算法的模型参考优化整定策略。
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