记作业>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。
      • For the aircraft with moderate swept wing, the main reasons of causing wing rock are the variations of roll damping moment with the angle of attack and the sideslip angle.
        对具有中等后掠角机翼的飞机,产生机翼摇晃的主要原因是滚转阻尼力矩随迎角和侧滑角的变化。
      • 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。
      • 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。
      • 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。
      • This paper introduces two methods to get the virtual sensor signal of angle of attack and sideslip angle: Nonlinear Observer method and INS/ GPS method.
        本文介绍了两种方法来得到迎角和侧滑角的虚拟传感器信号:非线性观测器方法和利用INS/GPS系统数据估计迎角和侧滑角方法。
      • 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。
      • 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
      • 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。
      • 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