N头条>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

      • 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
      • 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。
      • 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。
      • 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。
      • 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
      • 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。
      • 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
      • 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
      • 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。