1.
Numerical Research of Rolling Characteristics on Canard Missiles by Distance between Fin and Wing
鸭式导弹舵翼面间距影响滚转的数值研究
2.
Aerodynamic Characteristic Computations on Iced Airfoils、Multi-Element Airfoil and Rudder;
结冰后翼型、多段翼型及舵面的气动特性计算
3.
A control surface on an airplane that combines the functions of an elevator and an aileron.
升降副翼兼有升降舵和副翼两种功能的飞机控制平面
4.
Pull the servo extension cord out of the middle hole above the wing, for later use.
舵机延长线从机翼上面中部的孔中用预留的线绳拉出备用。
5.
Influence of Control Surface Characteristics on Short Period Mode Flying Qualities for Flying Wing Aircraft
舵面特性对飞翼构型作战飞机短周期品质的影响
6.
Study of Main/Flap Rudders Intelligent Coordinated Control for Ship Course-keeping;
舰船航向—舵/翼舵智能协调控制研究
7.
The plane systems and functions are also recorded, along with information about engine thrust and the position of control surfaces (flaps and rudder).
同时，它也记录飞机的系统和运行情况，包括发动机的推力和操纵面位置（襟翼和方向舵）。
8.
Aileron servo pull rod should be vertical to the shaft of aileron basically.
副翼舵机拉杆应基本上垂直于副翼转动轴线。
9.
Research of Calibration Technology on Angular Displacement for Elevator, Aileron and Flap of Airplane;
飞机升降舵、副翼和襟翼转角标定技术研究
10.
Repeat but use left cyclic instead of right cyclic.
重覆以上的动作，但是将副翼打左舵。
11.
Design and installation of 4000 DWT multi-purpose carrier flapped rudder
4000DWT多用途船襟翼舵的设计与安装
12.
Technology for welding flap helm with lower helm bearing of Changjiang roll-on-roll-off ship No.1
“长江重件1号”滚装船襟翼舵大齿轮与下舵承本体外圈的焊接技术
13.
flight control surface actuator
操纵面致动装置舵机
14.
Time the input of the cyclic& collective commands such that the helicopter path is that of a loop.
安排副翼、降舵及主旋翼螺距的打舵时机，使得直升机的飞行轨迹形成一个圆圈。
15.
Repeat the above steps, but start the maneuver by rolling to the right, and exit by rolling to the left.
重覆执行步骤1、及3，但将副翼打右舵执行1/侧滚。结束时将副翼打左舵。
16.
Repeat steps1&2, but this time roll the helicopter to the right( away from the pilot). Exit by rolling back to the left.
重覆执行步骤1及2，但将副翼打右舵执行1/侧滚（离操控者）结束时将副翼打左舵。
17.
Time the input of the cyclic& collective commands such that the helicopter maintains constant altitude, direction& speed.
安排副翼、降舵及主旋翼螺距的打舵时机，使得直升机能保持固定的高度、进方向及速度。
18.
Roll back to the right to exit this maneuver.
将副翼打右舵，使直升机恢复成为水平飞行。