The results of spacecraft space debris shield configuration, as well as pressure vessel damage behavior characteristic under hypervelocity impact conditions are presented as applications.
作为应用的例子给出了超高速撞击条件下航天器空间碎片防护结构以及压力容器损伤特性实验研究的结果。
2
This paper discusses the problem of detumbling a rigid spacecraft with an incomplete configuration of one sided thruster.
本文讨论了以非完整配置的单向推力器系统为执行机构时，刚性航天器的去翻滚控制问题。
3
The single gimbal control moment gyro (SGCMG) configuration of a large spacecraft is studied. First, the research object of analyzing configuration is restricted.