| 1. | These methods are applied to shenzhou manned spacecraft recovery system . some useful conclusions are gained by a simulation , which provide references for the stability analysis of manned spacecrafts in steaty decent 并将此分析方法运用于“神舟”号载人飞船的回收着陆系统,通过仿真分析得到一些有意义的研究结论,为载人飞船在稳定下降阶段的稳定性分析提供了参考。 |