1.
Control Surfaces Efficiency Analysis of Flexible Aircraft Based on Experimental Aerodynamic Forces
基于试验气动力的弹性飞机舵面效率分析
2.
A Simple Adaptive Reconfigurable Control Method for Aircraft Control Surface Loss-of-Effectiveness Failures
飞机舵面损伤的简单自适应重构控制方法
3.
the horizontal surface of an aircraft's tail assembly that is fixed and to which the elevator is hinged.
固定的连着升降舵的在飞机尾部的水平面。
4.
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
5.
Composite material repair for various structural parts of aircraft, such as Radome, flight control surface, etc.
雷达罩、操作舵面等飞机部件日常复合材料修理工作.
6.
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
7.
Load Simulator Design and Ground Test of Near Space Hypersonic Vehicle
近空间高动态飞行器舵机加载模拟器地面试验研究
8.
flight control surface actuator
操纵面致动装置舵机
9.
the horizontal stabilizer and elevator in the tail assembly of an aircraft.
飞机尾部的水平稳定器和升降舵。
10.
Calibration Method for Rudders Angular Displacement Based on Monocular Vision
标定飞机方向舵角位移的视觉测量法
11.
Electric Loading Test System for Aircraft Rudder
飞行器舵机电动加载测试系统的研究
12.
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）。
13.
Theoretical analysis and simulation results for fighter's control surface faults show that the presented method is effective.
理论分析和针对歼击机在机动飞行过程中各种舵面故障的仿真研究均表明本文方法的有效性。
14.
a lever used by a pilot to control the ailerons and elevators of an airplane.
飞行员用来控制飞机升降舵和副翼的杠杆。
15.
Aircraft actuator system failure can be detected by analytic redundancy analysis.
飞机舵机系统的机械故障可用解析余度法检测。
16.
Dynamic Simulation for Tailplane Actuater Servo System by Simulink
基于Simulink的飞机平尾舵机伺服系统动态仿真
17.
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。
18.
Novel Hybrid Magnetic Helm Actuator of Micro-Aircraft
微型飞行器新型极化电磁驱动舵机的研究