yawing

英 [ˈjɔːɪŋ]

美 [ˈjɔːɪŋ]

v.  偏航
yaw的现在分词

现在分词：yawing　

柯林斯词典

• VERB （飞机或船）偏航，偏离航线
  If an aircraft or a shipyaws, it turns to one side so that it changes the direction in which it is moving.
  1. As the plane climbed to 370 feet, it started yawing...
     飞机攀升到370英尺时，开始偏航。
  2. He spun the steering-wheel so that we yawed from side to side.
     他急速打着舵轮，把我们搞得摇来晃去的。

双语例句

• In each mode, it includes four attitude controls: rolling, pitching, yawing and thrust.
  在各种飞行模式下包含有四种姿态控制：滚动、俯仰、偏航和升降。
• Among most factors affecting the real-time image synthesis, attitude aberration caused by missile's attitudes such as yawing, pitching and rolling is one of key aberration models.
  在影响下视景象实时图像成像的各种误差因素中，导弹偏航、俯仰和翻滚等姿态引起的成像姿态畸变是其关键的畸变误差模型之一。
• In the paper, the relation between cable vibration acceleration and wind velocity, wind yawing anger, anger of attack are discussed. Nonstationarity in wind-rain induced response is studied, and the cause of this nonstationarity is discussed by using a wavelet approach.
  分析了拉索振动加速度信号与风速、风偏角以及风攻角的相关性；研究了斜拉索振动加速度信号的非平稳性，并使用小波分析的方法探讨了导致其非平稳的原因。
• This paper describes the characteristics of rotating and yawing damping moment of wraparound fins in sub-supersonic flow and theoretically proves the necessity of positive-opposite rotation of wraparound with thickness at zero angle of attack in sub-supersonic flow.
  本文给出了亚、超音速弧翼的滚转及偏航阻尼力矩特性，并从理论上证明了零攻角时有厚度弧翼在亚、超音速绕流时正、反向滚转的必然性。
• A Study of Mathematical Model for Yawing at Anchor
  锚泊偏荡运动数学模型的研究
• The research shows, in the process of hard grounding a considerable part of ship's initial kinetic energy turns into energy of revolving mode, which includes pitching, rolling and yawing.
  研究表明，在船舶高能搁浅动力学过程中，有相当部分的初动能转化为旋转形式的动能，包括纵摇、横摇和艏摇；
• The variation tendencies of the side force, rolling moment and yawing moment of the overtaking cars by two spaces are different apparently.
  超车车辆受到的侧向力、侧倾力矩和横摆力矩在两种间距下的变化趋势有着明显差别。
• Thirdly, by neglecting the coupling influence, the control laws of pitching, yawing and sloping movements are designed separately with frequency domain analysis and root locus, and then the parameters of the controller are chosen.
  第三，忽略耦合影响，将控制系统分为俯仰、偏航、倾斜三个相互独立的通道，用频域分析法和根轨迹法设计控制律、选取控制器参数。
• Firstly, we apply a method of classical gain scheduling to design attitude stable system of three channels including pitching, yawing, rolling.
  首先，采用古典的增益调度方法分别设计俯仰、偏航和滚转三个通道的姿态稳定系统和自动驾驶仪。
• The yawing can apparently attenuate the angular displacement of both the tail and the attack angle of tail fin.
  艏摇的存在会明显的衰减尾柄主臂和尾鳍攻角的角位移。