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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桨叶变距拉杆操纵载荷是旋翼设计的重要参数之一。

The pitch link loads of blade is one of the most important parameters in rotor design.

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桨叶变距拉杆操纵载荷是旋翼设计的重要参数之一。

The pitch link loads of blade is one of the most important parameters in rotor design.

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