This paper is about the study of realization of the target satellite interception method with velocitygain guidance.
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。
2
In this paper, the precise initial guidance law based on velocitygain guidance and the state transition matrix for orbit interception were proposed.
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。
3
A gait velocitygain that results in a transition to a higher class of ambulation results in better function and quality of life, especially for household ambulators.