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

• 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。
• 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。
• 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。
• Yawing moment of inertia of sprung mass
  簧上质量横摆惯性矩
• 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。
• 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。
• 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。
• 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。
• 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。