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

• 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
• 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。
• 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。
• As the plane climbed to 370 feet, it started yawing
  飞机攀升到370英尺时，开始偏航。
• 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。
• A Study of Mathematical Model for Yawing at Anchor
  锚泊偏荡运动数学模型的研究
• 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。
• 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 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。
• 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。