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
- 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。 - And this paper also using the 3-D vehicle model and the tire model studies the sideslip when the vehicle driving up or down.
运用车辆动力学模型和轮胎模型对汽车上、下坡行驶时的侧滑进行了研究。 - Engineering Test Method for Motor Vehicle Yaw Rate and Sideslip Angle Based on GPS Technology
基于GPS的汽车横摆角速度和侧偏角工程测试方法 - 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。 - 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。 - 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。 - 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。 - 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。 - Both the sideslip angle and the rudder angle are seen to be very much dependent on the angle of climb.
人们可以看到，侧滑角和方向舵偏角都在很大程度上依赖于爬升角。 - 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。