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

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