本文对运用速度增益制导实现对目标卫星的拦截方法进行了研究。

This paper is about the study of realization of the target satellite interception method with velocity gain guidance.

youdao

对于轨道拦截问题，给出了一种基于速度增益制导和状态转移矩阵的精确初制导方法。

In this paper, the precise initial guidance law based on velocity gain guidance and the state transition matrix for orbit interception were proposed.

youdao

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。

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.

youdao