词语屋>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

      • 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。
      • 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
      • 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
      • 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。
      • 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 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。
      • 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
      • 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。
      • 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;
      • 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。