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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

      • An Estimation Method of Angle-of-attack and Sideslip Angle Based on INS
        一种基于INS的攻角和侧滑角测量算法
      • 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
      • This method can be applied to calculate rolling-moment derivatives of wing due to yaw and sideslip.
        使用RBF神经网络气动模型提取气动导数本方法可以用来计算机翼因偏航与侧滑振动而引起的滚转力矩气动导数。
      • The safety analysis on the automobile braking deflection and sideslip
        汽车制动跑偏和制动侧滑安全分析
      • Valuation of Some Game-Type Option with Nonconstant Volatility Numerical Calculation of Aerodynamic Force Coefficient and Dynamic Stability Derivatives on Unsteady Supersonic Wing with Sideslip Angles
        波动率非常数时一类博弈期权的定价非定常超音速侧滑机翼的气动力系数及动导数的数值计算
      • Principle and method of data fusion are introduced firstly, then principle of utilizing the method of multisensor data fusion to estimate angle-of-attack and sideslip angle is studied, and verified by simulation finally.
        先介绍了数据融合的理论及方法,接着研究了利用多传感器数据融合方法来估计迎角和侧滑角的原理和方法,最后通过仿真进行了验证。
      • 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。
      • 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。
      • 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
      • 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。