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

• 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。
• 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。
• 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。
• Analysis the components of yawing system, and the process of a circular route of oil.
  对于偏航系统，分析了偏航系统的组成，液压控制偏航系统的油液循环路线的过程。
• 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 aerostatic bearings of minimum friction are used in two yawing measuring sets of the dynamometer. The power developed by turbine and the mechanical power lost in the turbocharger can be separately measured simultaneously.
  该测功机采用摩擦阻力最小的空气静压轴承作为两个测量机构的摆动轴承，能同时分别测出涡轮发出的功和涡轮增压器损失的机械功。
• A Study of Mathematical Model for Yawing at Anchor
  锚泊偏荡运动数学模型的研究
• 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。
• 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。
• 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；