得出的结论对研究人-电传操纵系统-飞机组合系统的驾驶员诱发振荡问题也是有益的。
These results are also useful in the study of the PIO problem of "men-Fly by control system-aircraft" synthetic system.
为了解决传统电传操纵系统抗电磁干扰能力差、带宽低等问题，提出了飞行控制系统光传方案。
A fly-by-light flight control system was developed to replace the fly-by-wire system which is susceptible to electromagnetic interference and has low bandwidth.
在航空航天飞行器设计中，随着主动控制技术、随控布局及电传操纵系统的普遍采用，飞行控制系统的地位变得更为重要。
With widespread adopting of the Active Control Technique(ACT) and Control Configuration Vehicle(CCV)and Fly-by- wire system, position of Flight ControlSystem(FCS) become even more significant.
飞行操纵系统的监控和冗余、飞机传感器、动力和液压的产生，这些构成了高度有效性的电传操纵。
Monitoring and redundancy within the flight control system, aircraft sensors, power and hydraulic generation ensure a high degree of availability of the electrical control.
该系统对飞机实施全权限数字电传操纵，可以在飞行中改变飞机的操纵感觉特性、操纵系统特性和纵向短周期气动特性。
The system adopts full authority DFBW for aircraft, which may change the characteristics of control feel, handling system and longitudinal short-period aerodynamics during flight.
该系统对飞机实施全权限数字电传操纵，可以在飞行中改变飞机的操纵感觉特性、操纵系统特性和纵向短周期气动特性。
The system adopts full authority DFBW for aircraft, which may change the characteristics of control feel, handling system and longitudinal short-period aerodynamics during flight.
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