location: Current position: Home >> Scientific Research >> Paper Publications

Active vibration control of flexible appendages of spacecraft during attitude maneuver

Hits:

Indexed by:会议论文

Date of Publication:2018-01-01

Page Number:1-6

Pre One:基于飞行路径角规划的再入参考轨迹设计方法

Next One:基于二级倒立摆的现代控制理论课程设计