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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

      • 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。
      • 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。
      • 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;
      • This paper describes a method of angle of sideslip calibration using a fuzzy neural network model.
        叙述了一种利用模糊神经网络模型来校正侧滑角的方法。
      • 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。
      • 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。
      • 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。
      • 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。