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航天器交会中的多圈Lambert问题研究
引用本文:谭丽芬,闫野,周英,唐国金.航天器交会中的多圈Lambert问题研究[J].国防科技大学学报,2010,32(5):12-16,28.
作者姓名:谭丽芬  闫野  周英  唐国金
作者单位:国防科技大学航天与材料工程学院;
基金项目:国家863高技术资助项目
摘    要:针对大椭圆轨道追踪器固定时间直接碰撞交会问题,介绍了一种快速确定多圈Lambert问题最优解的新方法。研究了多圈Lambert转移解,分析了转移时间与转移轨道参数的关系;研究了无时间约束最优直接碰撞交会及其必要条件。仿真表明:最优解快速确定方法有效、可行,并可提高计算效率。

关 键 词:多圈Lambert转移  最优交会  大椭圆轨道
收稿时间:4/2/2010 12:00:00 AM

Research on Multiple-revolution Lambert Problem in Spacecraft Rendezvous
TAN Lifen,YAN Ye,ZHOU Ying and TANG Guojin.Research on Multiple-revolution Lambert Problem in Spacecraft Rendezvous[J].Journal of National University of Defense Technology,2010,32(5):12-16,28.
Authors:TAN Lifen  YAN Ye  ZHOU Ying and TANG Guojin
Institution:TAN Li-fen,YAN Ye,ZHOU Ying,TANG Guo-jin(College of Aerospace and Material Engineering,National Univ.of Defense Technology,Changsha 410073,China)
Abstract:According to the fixed-time hard rendezvous with chase spacecraft in high eccentric orbit,a new algorithm was introduced to solve multiple-revolution Lambert problem,which can find the optimal transfer orbit quickly.The solutions of multiple-revolution Lambert transfer problem were researched,and the relationship between transfer time and transfer orbit elements was figured out while the optimal rendezvous problem without time constraint was also studied.The calculation results for fixed-time rendezvous val...
Keywords:multiple-revolution lambert transfer  optimal rendezvous  high eccentric orbit  
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