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
• 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。
• 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。
• 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。
• 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
• 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。
• 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。
• The research shows, in the process of hard grounding a considerable part of ship's initial kinetic energy turns into energy of revolving mode, which includes pitching, rolling and yawing.
  研究表明，在船舶高能搁浅动力学过程中，有相当部分的初动能转化为旋转形式的动能，包括纵摇、横摇和艏摇；
• 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。