航天器工程2024，Vol.33Issue(1)：19-25,7.DOI:10.3969/j.issn.1673-8748.2024.01.003
空间站舱段平转式转位方案设计与验证
Design and Verification of Space Station Module Flat Transfer Scheme
罗超 1罗文成 1刘冬雨 1史纪鑫1
作者信息
- 1. 北京空间飞行器总体设计部,北京 100094
- 折叠
摘要
Abstract
According to the mission requirement that the direction of China Space Station labora-tory module to the sky or the earth should remain unchanged before and after transfer,a flat transfer scheme is proposed in this paper,and a module transfer implementation scheme based on flat transfer mechanism is designed.During the module transfer,a passive gravity gradient stable attitude is taken by space station for flight,which enables the space station to stabilize its own di-rection when it stops active attitude control.By designing and selecting appropriate transfer mis-sion window,it can ensure unblocked track telemetry control link and sufficient sunlight during the whole transfer process,improving the mission security and reliability.Through ground tests and orbital laboratory module transfer missions implementation,the space station module flat transfer scheme has been comprehensively verified.关键词
空间站/组装建造/平转式/转位机构Key words
space station/assembly and construction/flat transfer/transfer mechanism分类
航空航天引用本文复制引用
罗超,罗文成,刘冬雨,史纪鑫..空间站舱段平转式转位方案设计与验证[J].航天器工程,2024,33(1):19-25,7.
