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。
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。
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