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

• And the turning radius and angle are obtained from the yawing angle information and the odometer information of the three wheels using fuzzy fusion technology.
  利用移动机器人三个轮子的里程信息和导向轮的转角信息，通过信息模糊融合获得转弯半径和转角，再利用运动学模型获得机器人的位置和方向。
• The pupils model themselves upon their teacher. Hydrodynamic Simulation and Analysis of Yawing of Bionic Robot Fish
  小学生仿效他们的老师。仿生机器鱼艏向摆动动力学仿真及分析
• 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。
• The normal force, pitching and yawing moments on the fuselage in hover result from the rotor downwash.
  悬停时，下洗尾流使机身产生负升力、俯仰力矩和偏航力矩。
• 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。
• Yawing moment of inertia of sprung mass
  簧上质量横摆惯性矩
• Physical model experiments were made to obtain the observed data of yawing range, yawing period and mooring force of3 ship types under different working conditions.
  通过物理模型试验，得到了3种船型在不同工况组合下的偏荡幅度、偏荡周期以及系泊力实测数据。
• The range of yawing rate when turning left in hover is calculated, where the tail rotor might get into vortex ring.
  根据右侧飞试验结果，估算出样机悬停回转时尾桨处于涡环状态的偏航角速度范围；
• 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。
• As the plane climbed to 370 feet, it started yawing
  飞机攀升到370英尺时，开始偏航。