字典二二>英语词典>sideslip翻译和用法

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

      • 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
      • 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 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。
      • Nonlinear supersonic potential flow over sideslip conical bodies delta wings and fuselages
        绕侧滑锥体、三维机翼与机身的超音速非线性全位势流计算
      • 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
      • This paper describes a method of angle of sideslip calibration using a fuzzy neural network model.
        叙述了一种利用模糊神经网络模型来校正侧滑角的方法。
      • 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
      • 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。
      • 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。