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

• A Study of Mathematical Model for Yawing at Anchor
  锚泊偏荡运动数学模型的研究
• 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。
• They were subject to violent yawing at low wind speeds.
  它们在低风速下会发生强烈的偏离。
• Combined with the characteristic of vehicle walking mechanism and track line, the geometry relation and dynamics relation among air spring, yawing and tack is described with mathematical formulas.
  结合车辆走行机构和线路轨道的结构特点，对空气弹簧、转向架和轨道之间的几何关系和动力学关系进行了数学描述。
• In order to reveal the cause and mechanism of the vibrations, a torsional vibration model of tower was set up based on the structure and principle of the yawing system.
  根据风力机偏航系统的结构和偏航原理，建立塔架扭转振动的模型。
• 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。
• Modeled the regulating mechanism by adjusting the pitch of blade and yawing system with first-order model.
  采用一阶模型对风力机变桨距机构和偏航机构建模。
• Hydrodynamic Simulation and Analysis of Yawing of Bionic Robot Fish reciprocating power-driven tine harrow
  仿生机器鱼艏向摆动动力学仿真及分析动力驱动摆动式钉齿耙
• By comparison and analysis of a large number of measured data, revealing the yawing motion of the FPSO is the main reason for this phenomenon.
  通过对大量的实测数据进行比较和分析，揭示了FPSO的艏摇运动是产生这种现象的主要原因。
• When twin vertical fins are located at the wing surface the maximum lift coefficient could be increased obviously and the incidence range of yawing and rolling stability is extended.
  当双立尾分别移到机身外侧置于机翼上时，可以显著提高全机最大升力系数，同时使航向和滚转稳定的迎角范围大为扩展。