飞机操纵系统是一个控制飞机飞行安全的关键系统。
Aircraft control system is a key system to ensure flight safety.
使飞机操纵系统和舱门能正常工作而做的装配调整。
An adjustment of airplane controls and doors for proper operation.
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.
典型的教练机训练效能计算模型对飞机的航空电子系统、操纵系统考虑不足，对飞行参数选择有局限性。
The typical computation model of training effectiveness of training plane has limitation in selection of flight parameters as well as insufficient attention to avionics and control system.
利勃海尔采用了可变液压操纵的设备作为A380飞机飞行操纵系统来驱动襟翼，这是这种理论第一次应用在航空领域。
For the A380's flight control systems, Liebherr has adopted equipment with variable hydraulic control to drive the wing flaps, the first time this principle has been used in aviation.
某型四余度电液舵机是飞机平尾操纵系统的关键部件，是机、电、液高度耦合的复杂系统。
One four redundant steering engines is a crucial component of aircraft stabilizer manipulative systems, and it is a complicated system related to mechanical, electrical and hydraulic elements.
研究了飞机发动机操纵系统地面模拟实验中用力矩电机进行电动加载控制问题。
Variable structure control was discussed for aircraft engine manipulating system simulator with motor loading.
在对某型飞机横向操纵系统分析基础上，列举出危害飞行安全的典型故障；
Based on the analysis of lateral-directional control system of a certain plane, representative fault infecting flying security is specialized;
飞行员说这架飞机对操纵系统反应不灵敏。
本文阐述了某型飞机发动机操纵系统地面模拟试验控制系统，它主要控制力矩电机去模拟油门杆上的速度和力以及模拟发动机输入轴的力矩。
This paper presents a simulation test control system of an airplane engine operating system, which control motor to simulate the force and velocity of throttle lever and the torque on axis.
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.
本文对高空超音速飞机中与增稳舵机交联的纵向机械操纵系统的力反传问题作了理论探讨。
This paper presents a. preliminary research on the feedback of feel of longitudinal mechanical control system connected with steering-engine in supersonic fighter.
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.
MA60飞机操纵负荷系统模拟飞机主操纵系统、辅助操纵系统、发动机的操纵(如油门杆)和刹车系统的操纵。
MA60 aircraft control system, simulating an aircraft in the main load control system, auxiliary system control, engine control (for example, under the accelerator) and brake control system.
MA60飞机操纵负荷系统模拟飞机主操纵系统、辅助操纵系统、发动机的操纵(如油门杆)和刹车系统的操纵。
MA60 aircraft control system, simulating an aircraft in the main load control system, auxiliary system control, engine control (for example, under the accelerator) and brake control system.
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