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.
然后飞机在自动驾驶仪的操控下飞几个小时，最后在800英尺以下，襟翼和起落架已经放下，由自动油门保持着速度，他解除自动驾驶操纵飞机着陆。
Then he might fly for hours on the autopilot and finally disengage it (MAYBE?) below 800 ft after the gear was down, flaps extended and on airspeed (autothrottle). Then he might bring it in to land.
襟翼周期变距操纵响应与传统旋翼类似。
The blade response of flap cyclic control is just similar to that of the conventional rotor.
根据襟翼电气操纵系统的通电故障，叙述了襟翼电气操纵系统功能、故障分析及线路改进过程。
According to electrify malfunction of flap electric operation system, the text depicts flap electric operation sys-tem function, malfunction analysis and circuitry improvement process.
建立了一整套更为合理、更为精确的系统安全性设计与分析技术。该技术已成功应用某机型襟翼操纵系统安全性设计与分析。
Finally, a more appropriate and accurate technological package for system safety analysis and design was established and applied to the system safety engineering of some airplane flaps successfully.
首先根据电控旋翼的刚体桨叶变距运动方程，推导了襟翼操纵量与桨叶桨距的显式关系式。
First, relationship between flap input and blade pitch was deduced based on the pitch kinetic equation of rigid blade.
首先根据电控旋翼的刚体桨叶变距运动方程，推导了襟翼操纵量与桨叶桨距的显式关系式。
First, relationship between flap input and blade pitch was deduced based on the pitch kinetic equation of rigid blade.
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