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 rudder plays a secondary role during a turn it is used to prevent yawing.
  在转弯时，方向舵发挥的作用仅次于离心力，方向舵用来防止偏航。
• 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。
• 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。
• In the paper, the relation between cable vibration acceleration and wind velocity, wind yawing anger, anger of attack are discussed. Nonstationarity in wind-rain induced response is studied, and the cause of this nonstationarity is discussed by using a wavelet approach.
  分析了拉索振动加速度信号与风速、风偏角以及风攻角的相关性；研究了斜拉索振动加速度信号的非平稳性，并使用小波分析的方法探讨了导致其非平稳的原因。
• 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。
• According to multivariable frequency design theory, this paper studies the coupling between a guided bombs yawing and rolling channels by relative gain.
  文中从制导炸弹的侧向扰动运动方程出发，根据多变量频率设计理论，用相对增益法，研究了制导炸弹航向和滚转通道的交联耦合。
• 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；
• 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