sideslip
英
美
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
双语例句
- 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; - 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 - 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。 - 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。 - 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 - 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。 - In the controller, the assisted motor angle is controlled by the feedback of yaw rate and the sideslip angle.
并以转向盘转角、横摆角速度和侧偏角为优化目标,设计了线性二次型调节器控制。 - 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 - 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 - 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。