读知识>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

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