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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 order to enhance stabilization, improve flight quality and maneuverability of the UAV, three methods for gaining two important feedback signals& angle-of-attack and sideslip angle that are needed in UAV control and stability augmentation system are studied in this dissertation.
        本文以提高无人机在各种状态下的稳定性和机动性、改善飞行品质为目标,研究了无人机控制增稳系统所需要的两个重要的反馈信号&迎角和侧滑角的三种获取方法。
      • For wings of arbitrary plan forms, sideslip aerodynamic characteristics have been calculated numerically and compared with experimental values.
        对几种平面形状的机翼侧滑气动力特性进行了数值计算,并与实验作了比较。
      • Yaw and Sideslip Control for Light Vehicle with Electromechanical Brake System
        轻型电子机械制动汽车横摆与侧偏控制研究
      • 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。
      • Vehicle Sideslip Angle Estimation Under Extreme Driving Condition Application of DMO analysis in 3-D geometry design
        极限行驶条件下车辆质心侧偏角观测器设计倾角时差校正在三维观测系统设计中的应用
      • 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
      • Estimation of CG Sideslip Angle Based on Extended Kalman Filter
        基于扩展卡尔曼滤波的汽车质心侧偏角估计
      • 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。
      • 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。
      • 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。