1) fault-tolerant flight control systems
容错飞行控制系统
3) fault-tolerant aviation control system
容错飞控系统
4) active fault tolerant flight control
主动容错飞行控制
1.
Integrated active fault tolerant flight control based on RMMAC
基于RMMAC的集成主动容错飞行控制
5) fault-tolerant control system
容错控制系统
1.
This paper studies a fault-tolerant control system for a space modular manipulator system mounted on space station or other spacecrafts such as satellites, located in low earth orbit.
研究搭载在空间站或其他近地轨道航天器上的空间模块化机械手系统的容错控制系统。
2.
The need of simultaneous stabilization or pole-assignment is due to de-signing fault-tolerant control systems.
同时稳定或极点配置是出于设计容错控制系统之所需。
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：容错
1.亦作"容厝"。亦作"容措"。 2.犹措置;安放。
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