52古典>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

      • 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。
      • 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
      • 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。
      • 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。
      • Truncated streamtraced inlet is sensitive to the flight at angles of attack or sideslip.
        截短流线跟踪进气道对带攻角或侧滑角飞行比较敏感。
      • 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
      • 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。
      • And this paper also using the 3-D vehicle model and the tire model studies the sideslip when the vehicle driving up or down.
        运用车辆动力学模型和轮胎模型对汽车上、下坡行驶时的侧滑进行了研究。
      • From the result, some research has been done to find out the different between sideslip angle sliding-mode control and yaw rate sliding-mode control.
        通过仿真结果着重研究了横摆角速度滑模控制和质心侧偏角滑模控制的特性;
      • 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。