The simulation results shows that lateral attitude control system has good control performance and the auto-trim control strategy plays a effective role.
仿真验证结果表明，抗不确定干扰的横侧向姿态控制回路控制性能良好，自动配平控制策略能有效发挥作用。
The paper also describes a ground demonstration of a one channel primary flight control system and a flight demonstration of an aileron trim control system.
同时还介绍了一单通道主飞控系统的地面演示和一副翼配平控制系统的飞行演示。
You have full control over when the next polling occurs, so it's possible to trim the values should the load on the server increase.
您可以完全控制进行下一次轮询的时间，因此完全有可能调整服务器负载应增加的值。
Many airplanes have trim for bank control, called aileron trim.
许多飞机有修剪为银行控制，叫的飞机辅翼修剪。
Pitch axis - Horizontal or lateral axis, passes through the airplane from one side to the other - nose up and nose down control is by elevators (and stabilizer for trim).
俯仰轴—又称水平轴或横轴。由飞机的一侧通向另一侧。飞机绕此轴转动即造成机首的俯与仰。俯仰控制是由升降舵来达成的，水平安定面则为配平之用。
T rim: trim to relieve control pressure and maintain attitude. DO NOT use the trim to adjust the attitude.
调整片：利用调整片减少杆力并保持姿态。禁止利用调整片直接进行姿态调整。
An operational check of the trim, controllability, or other flight characteristics to establish that the production aircraft has the same range and degree of control as the prototype aircraft.
配平、操纵性、或者其他飞行特性的操纵检查，以确定量产型飞机与原型飞机有着相同的程度和范围的操纵性能。
Interior trim data control model is divided into two parts, i. e. absolute base data control model and relative base data control model.
内饰数据控制模型划分为绝对基准数据控制模型和相对基准数据控制模型。
V-port trim has a more linear throttling curve than plug or ball discs, but none of these trims are recommended for continuous severe throttling which may require using a control valve.
形端口阀内件截止阀比塞形阀瓣或球形阀瓣截止阀具有更加线性的节流曲线，但是，所有这些类型的截止阀都不建议连续用于严格的节流应用中，这种情况可能需要采用控制阀。
Horizontal or lateral axis, passes through the airplane from one side to the other - nose up and nose down control is by elevators (and stabilizer for trim).
从飞机一侧通向另一侧的水平轴或横轴。升降舵控制机头绕此轴作上下的运动。(水平安定面则用以配平。)
Research on the trim and control characters of the helicopter was conducted, which featured with the electrical controlled rotor (ECR).
对采用电控旋翼直升机的配平及操纵特性进行了研究。
Finally, the control stability was discussed and it was found out that trim Angle control is a simple and effective method to make the submersible stable near the free surface.
对控制稳定性进行了讨论，发现纵倾角控制是使潜体近水面稳定的一种简单而有效的方法。
The control valves with ceramic trim are expounded. It has the corrosion-proof, abrasion-proof and high temperature proof performance, and it also has obtained successful application.
论述了陶瓷内件控制阀的研制，该阀内件同时具有耐腐蚀、耐磨损(包括冲刷、气蚀)与耐高温的性能。已获得成功应用。
When the autopilot is disengaged, the control wheels and ailerons move to the (possibly undesired) neutral point and the airplane will roll proportional to the amount of trim input.
一旦自动驾驶被脱开，操纵盘和副翼就移向新的(可能是不需要的)中立点，并且，飞机将与配平输入量成比例地滚转。
When the autopilot is disengaged, the control wheels and ailerons move to the (possibly undesired) neutral point and the airplane will roll proportional to the amount of trim input.
一旦自动驾驶被脱开，操纵盘和副翼就移向新的(可能是不需要的)中立点，并且，飞机将与配平输入量成比例地滚转。
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