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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

      • 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。
      • 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
      • 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
      • 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;
      • 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。
      • Engineering Test Method for Motor Vehicle Yaw Rate and Sideslip Angle Based on GPS Technology
        基于GPS的汽车横摆角速度和侧偏角工程测试方法
      • Results show that sideslip makes twisting of vortices at upwind side delayed, but bursting of.
        研究表明,侧滑使机翼迎风侧涡绞合推迟,涡提前破裂,背风侧正好相反。
      • 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。
      • 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。
      • Numerical Calculation of Aerodynamic Force Coefficient and Dynamic Stability Derivatives on Unsteady Supersonic Wing with Sideslip Angles
        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