1.
Design and Implement of Four Redundancy Helming Mechanism Control System
四余度舵机控制系统的软件平台架构与实现
2.
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。
3.
A Research and Design of Entire Dual Redundancy Electro-Mechanical Actuator
完全双余度电动舵机系统的研究与设计
4.
The Simulator Design of the Four-channel Electro-hydraulic Servo Actuator
某型飞机电传操纵系统四余度电液舵机模拟器设计
5.
Applied Research on the Electro Hydraulic Redundancy Digital Valve in Marine Hydraulic Steering Gear
电液余度数字阀在船舶液压舵机系统中的应用研究
6.
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。
7.
Calculation and Analysis of Accumulator for the Test of the Impedance of Hydraulic Booster Location System
舵机动刚度试验台蓄能器的计算与分析
8.
High-precision Electromechanical Actuator Cascade Control Based on Robust H_∞ Optimization
基于鲁棒H_∞优化高精度导弹舵机串级控制研究
9.
With the helicopter hovering Tail-In pull back cyclic, and work the collective to complete at least two (2) full back tumbles while maintaining a constant altitude and heading.
机尾朝向操控者保持停悬，将升降舵拉升舵使直升机保持固定的高度及方向，向后翻滚至少二圈。
10.
With the helicopter hovering Nose-In pull back cyclic, and work the collective to complete at least two (2) full back tumbles while maintaining a constant altitude and heading.
机头朝向操控者保持停悬，将升降舵拉升舵使直升机保持固定的高度及方向，向后翻滚至少二圈。
11.
length-balance ratio
舵平衡部分长度与舵总长度之比
12.
While maintaining a constant altitude use the tail rolor to rotate the helicopter clockwise90 degrees, hold for ten(10) seconds.
保持稳定的停悬高度，将方向舵打右舵，使直升机顺时针旋转90°保持静止倒飞停悬10秒钟。
13.
automatic rudder control
自动舵机控制自动舵控制
14.
Leonard system steering
发电机电动机系统操舵
15.
Simulation on Ram-air Rudder Vibration Parameters Change With Flight Speed
冲压式舵机自振参数随飞行速度变化规律的仿真
16.
Position Control System for Ship Rudder Machine Base on H_Q Mixed Sensitivity Method
基于H_Q混合灵敏度控制的船用舵机位置伺服系统研究
17.
Hydraulic steering gear on the inland navigation ships
GB/T7185-1987内河船液压舵机
18.
flight control surface actuator
操纵面致动装置舵机