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
- Estimation of CG Sideslip Angle Based on Extended Kalman Filter
基于扩展卡尔曼滤波的汽车质心侧偏角估计 - 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。 - 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。 - 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 - 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。 - 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 - 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。 - 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。 - 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