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sideslip

网络  横滑; 侧滑; 侧滑角

现在分词:sideslipping 过去式:sideslipped 

COCA.47059

英英释义

noun

  • a flight maneuver
      Synonym:slip
    1. an unexpected slide
        Synonym:skidslip

      双语例句

      • In most flight conditions it is desired to maintain the sideslip angle equal to zero.
        大多数飞行状态都要求保持侧滑角等于零。
      • Lifting surface theory and the numerical method of wings with small angles of sideslip at subsonic and supersonic speeds
        亚、超音速小侧滑角机翼升力面理论和数值计算方法
      • Engineering Test Method for Motor Vehicle Yaw Rate and Sideslip Angle Based on GPS Technology
        基于GPS的汽车横摆角速度和侧偏角工程测试方法
      • The observer using the coupling of axial and lateral and having feedback of acceleration is investigated. This method can estimate the angle of attack and the sideslip angle synchronously. An optimization named Extrem is applied to optimize the feedback plus matrix.
        研究了采用纵横向耦合且具有线加速度反馈的非线性观测器方法,该方法能够同时估计迎角和侧滑角参数,并采用Extrem优化方法对其反馈参数增益参数进行了优化设计。
      • Both the sideslip angle and the rudder angle are seen to be very much dependent on the angle of climb.
        人们可以看到,侧滑角和方向舵偏角都在很大程度上依赖于爬升角。
      • Results show that sideslip makes twisting of vortices at upwind side delayed, but bursting of.
        研究表明,侧滑使机翼迎风侧涡绞合推迟,涡提前破裂,背风侧正好相反。
      • Based on a zero sideslip angle proportional control, we get the gain of the distance from the centroid to the steering center position, yaw angular velocity and lateral acceleration.
        在此基础上,得到车辆采用零侧偏角控制策略时,车辆转向中心到质心的距离,横摆角速度增益及侧向加速度增益的表达式。
      • Study of Urban-rural Gap in China from the Perspective of Urban-oriented Policies Vehicle Sideslip Angle Estimation Under Extreme Driving Condition
        城市偏向政策视角下我国城乡差距问题研究极限行驶条件下车辆质心侧偏角观测器设计
      • In the controller, the assisted motor angle is controlled by the feedback of yaw rate and the sideslip angle.
        并以转向盘转角、横摆角速度和侧偏角为优化目标,设计了线性二次型调节器控制。
      • In this paper, under the basic assumptions of sideslip angle to zero and aircraft moment balance, the motion equations are established.
        本文基于侧滑角为零和作用在飞行器上的力矩平衡的基本假设条件下,建立运动方程。