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载人航天器低空应急救生分离时刻计算
引用本文:曾国强,任萱.载人航天器低空应急救生分离时刻计算[J].中国空间科学技术,2000,20(3):49-53.
作者姓名:曾国强  任萱
作者单位:国防科技大学航天与材料工程学院,长沙
摘    要:讨论了载人航天器低空应急救生时返回舱与逃逸飞行器分离时刻Ta的计算方法。首先推导了逃逸弹道的近似解;然后提出了基于近似解的返回舱与逃逸飞行器分离时刻Ta的实时确定方法;最后,仿真分析了该方法对提高载人航天器低空逃逸救生概率的作用,证明利用近似解实时求解分离时间Ta是一种简单实用、效果明显的方法。

关 键 词:载人飞船  舱段分离  载人航天器  返回舱  逃生

An Algorithm for Separation Time of Manned Spacecraft Emergency Rescue at Low Altitude
Zeng Guoqiang,Ren Xuan,Jia Peiran.An Algorithm for Separation Time of Manned Spacecraft Emergency Rescue at Low Altitude[J].Chinese Space Science and Technology,2000,20(3):49-53.
Authors:Zeng Guoqiang  Ren Xuan  Jia Peiran
Abstract:An algorithm for separation time T a of manned spacecraft reentry capsule from escape system is discussed.At first,an approximate solution of escape trajectory is deduced.Then,a real-time algorithm for separation time T a is presented,which is based on the approximate solution.Finally this simple algorithm is proved to be useful for increasing the probability of success of emergency rescue by numerical simulation.
Keywords:Manned spacecraft  Emergency recovery  Module separation  Time  Calculation method  
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