机翼和机尾上的可动面板，用以操纵飞机俯仰，坡度，和偏航运动。
Moveable panels on wings and tail for movement of airplane on pitch, roll and yaw axes.
操纵面，机翼和机尾上的可动面板，用以操纵飞机俯仰，坡度，和偏航运动。
CONTROL SURFACE, Moveable panels on wings and tail for movement of airplane on pitch, roll and yaw axes.
目标传感器安装在飞机俯仰和偏航运动的关键就硬性连接到机身身体万向节大会。
A target sensor is mounted for pivotal movement in the pitch and yaw planes on a gimbal assembly rigidly connected to the airframe body.
内环路控制，对于自动驾驶仪操作，这是无关飞行航道的飞机俯仰姿态和坡度的基本控制。
INNER LOOP control, For autopilot operation this is the basis control of airplane pitch and roll attitude without regard to flight path.
该算法在不增加系统硬件的前提下，充分利用液压缸现有行程，逼真地模拟飞机俯仰、滚转、偏航、升降、纵向和侧向平移运动。
On the basis of hardware in existence, the algorithm can make use of the journey and provide fidelity sense of pitch, roll, yaw, heave, surge and sway motion.
升降舵，铰连在水平安定面后缘上的可动部件。用以操纵飞机的俯仰运动(机头朝上及朝下)。
ELEVATOR, a hinged moveable part on the trailing edge of the horizontal stabilizer for airplane pitch (nose up and nose down) control.
移动升降舵离开它们的流线型位置，使得飞机改变水平轴上的俯仰姿态。
Moving the elevators out of their faired position causes the airplane to change the pitch attitude about the lateral axis.
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。
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).
参照失速速度修正方法给出了受俯仰操纵效能限制的飞机最小离地速度的修正方法；
The method of modifying the minimum unsticks speed for airplanes having the limited pitch control authority is also given referring to the method of modifying the stall speed.
用来显示飞机的俯仰姿态和坡度的电子显示。
An electronic display of airplane attitude information in pitch and roll.
本文用微分方程定性理论来分析俯仰力矩曲线随迎角变化的“勺形”对飞机飞行稳定性的影响。
The theory of stability of differential equations is used to analyse the 'effect of reversal slope of pitch moment to the stability of aircraft.
在理解飞机飞行品质规范MIL-STD- 1797A基础上，采用等效系统准则评价了某机的俯仰轴飞行品质。
The handing qualities of aircraft for pitch axis are assessed using equivalent system criteria based on the flying qualities specifications(MIL STD 1797A).
飞机尾翼的可动水平面，用来控制俯仰配平。
The moveable horizontal surface of the empennage used for pitch trim.
介绍在使用国军标规范《军用飞机强度和刚度规范》中对于急剧俯仰机动、滚转改出及滚转机动机翼载荷计算时所遇到的困难、解决办法及其软件研制。
The paper introduces the difficulties met in A/C loads calculation during abrupt pitching maneuver and rolling pullout, and in wing load calculation during rolling maneuvers.
应用该模型对某飞机模型做俯仰滚转耦合运动的非定常气动力进行了辨识。
Using the model the unsteady aerodynamics of one aircraft in pitching-rolling motion is identified.
数字摄像机安放在经纬仪上，经纬仪布置在飞机飞行轨迹的两侧，构成了一个能够在俯仰角和方位角下拍摄图像的光测机构。
The cameras are placed on the theodolites which are laid on the sides of flight path, and it can take airplane′s photos at azimuth and pitching angle.
本文为某型飞机设计了直接力两种模态——机身俯仰和垂直平移的控制器。
In the end of the paper, the controllers of pitch pointing and vertical translation modes are designed for an airplane. And the simulation results of two modes are excellent.
水平仪是飞机综合训练模拟器座舱仪表系统中用于显示飞机飞行姿态的仪表，主要完成俯仰、倾斜等指示功能。
Artificial horizon, an instrument of cockpit meter systems of the ACTE, is mainly used to indicate the flight attitude, such as pitching Angle and tilt Angle etc.
建立了飞机在随机跑道激励下，考虑机身俯仰运动与弹性振动的非线性随机动力学模型。
A nonlinear stochastic dynamic model is established which takes into consideration aircraft body pitch movements and the elastic vibration excited by the random runway.
建立了飞机在随机跑道激励下，考虑机身俯仰运动与弹性振动的非线性随机动力学模型。
A nonlinear stochastic dynamic model is established which takes into consideration aircraft body pitch movements and the elastic vibration excited by the random runway.
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