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载人航天器低空救生仿真
引用本文:郭叔伟,董杨彪,丁娣,秦子增.载人航天器低空救生仿真[J].国防科技大学学报,2008,30(4):22-27.
作者姓名:郭叔伟  董杨彪  丁娣  秦子增
作者单位:国防科技大学,航天与材料工程学院,湖南,长沙,410073
摘    要:在载人航天器低空救生中,回收系统开伞点的初始状态参数如速度、离地面高度、弹道倾角对返回舱能否安全着陆有很大影响.与正常返回类似,低空救生中的回收系统同样经过多级伞的拉直、充气、全充满等运动过程.通过建立回收系统着陆过程的动力学模型,经过大量仿真对比分析,得到开伞点离地面高度为低空救生中返回舱安全着陆的首要因素,同时对低空救生中回收系统多级伞开伞减速过程有了详细的分析.

关 键 词:载人航天器  低空救生  降落伞  返回舱
收稿时间:3/5/2008 12:00:00 AM

A Research on Simulation of Manned Spacecraft Rescue at Low Altitude
GUO Shuwei,DONG Yangbiao,Ding Di and QIN Zizeng.A Research on Simulation of Manned Spacecraft Rescue at Low Altitude[J].Journal of National University of Defense Technology,2008,30(4):22-27.
Authors:GUO Shuwei  DONG Yangbiao  Ding Di and QIN Zizeng
Institution:GUO Shu-wei,DONG Yang-biao,Ding Di,QIN Zi-zeng (College of Aerospace , Material Engineering,National Univ.of defense Technology,Changsha 410073,China)
Abstract:In the manned spacecraft rescue at low altitude,the initial conditions of recovery system at parachute-opening point affect obviously cabin safety landing,such as its velocity,altitude and trajectory angle.Similar to the normal return rescue,the process of recovery system rescue at low altitude also has the stages of deployment,inflation,and full-inflation of multilevel parachute.Through applying the recovery system landing dynamic model,and analyzing contrastively the results from simulation,it can be know...
Keywords:manned spacecraft  rescue at low altitude  parachute  cabin  
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