horizontal tail

Analysis of Active Control Technology Effect on Horizontal Tail Area

主动控制技术对平尾面积的影响分析

Reliability analysis of the transmission shaft of the all-moving horizontal tail for a fighter plane

歼击机全动平尾转轴梁的可靠性分析

According to the normal model of UAV, then the force and moment of the deadlock rudder are regarded as constant disturbance, the models of differential horizontal tail UAV and flying head tail UAV which are related to the spiral motion are established respectively.

然后以正常无人机模型为基础，把方向舵卡死产生的力与力矩当作常值扰动，分别建立了常规布局无人机和差动平尾无人机与螺旋运动相关的模型。

Method to Analyze Horizontal Tail Area Benefits of RSS Aircraft

放宽纵向静稳定度飞机的平尾面积收益分析方法

They note the vertical tail of the "bird" resembles a tailplane on an aircraft as opposed to the horizontal tail feathers of a real bird.

他们指出，该“鸟”的垂直尾部类似于飞机上的横尾翼，而与真正鸟类的水平尾羽方向相反。

Preliminary design of horizontal tail of subsonic civil aeroplane

亚音速民机平尾初步设计

In this paper, the transmission shaft of the all-moving horizontal tail for a fighter plane is considered as a structural system, and its failure probability is analysed.

本文从整个构件系统着眼，研究某型歼击机全动平尾转轴梁静强度的可靠性。

Study of the Lateral Model Adopt Differential Horizontal Tail and Rudder Effect

差动平尾和方向舵辅助滚转的横航向数学模型研究

Using the analytical relationship, many boundaries namely scissors sketed, could be drawn on the parameter plane of horizontal tail area and aeroplane center of gravity.

利用这种解析关系，可以在平尾相对面积和飞机重心位置的参数平面上，绘制出各种限制边界，形成所谓剪刀图。

Including the horizontal stabilizer fin ( horizontal tail ) and the vertical fin ( vertical tail ).

尾翼包括水平尾翼 ( 平尾 ) 和垂直尾翼 ( 垂尾 ).

Automatic Test of Aircraft Failure in Deflected Angle of Horizontal Tail

飞机平尾偏角故障的自动检测

The horizontal tail wing of the wing-in-ground effect craft has the advantages of great ascensional force, small area and low production cost.

这种地效翼船水平尾翼，升力大、面积小、生产成本低。

This paper are collected and expressed by the analytical relationship of horizontal tail area to aeroplane center of gravity.

本文着重搜集、归纳了那些重要的，且又便于在飞机初步设计阶段使用的品质要求，并将它们用平尾相对面积和飞机重心之间的解析关系表达出来。