航天器工程2011，Vol.20Issue(5)：11-36,26.
美国航天器交会技术研究
Study on Rendezvous Techniques of American Spacecraft
朱仁璋 1王鸿芳 2徐宇杰 1魏羽良3
作者信息
- 1. 南京大学,南京210093
- 2. 北京航空航天大学,北京100191
- 3. 中国空间技术研究院,北京100094
- 折叠
摘要
Abstract
The US rendezvous and docking techniques development can be divided into three stages： Gemini and Apollo spacecraft,Space Shuttle,and post-Shuttle projects.Progression of autonomous rendezvous technology is firstly based on developing various guidance and navigation sensors,in particular,laser sensors used during the final approach phase.Redundance in the Guidance,Navigation and Control system and fault detection and isolation method play an important role in trajectory safety.The projects being studied in this paper include Gemini,Apollo,Shuttle,post-Shuttle planned ones（Orion,Dragon,Cygnus,BlackSky,and on-orbit satellite servicing）,and flight demonstrations（XSS-11,DART and Orbital Express）,with focus on rendezvous trajectories and rendezvous sensors as well as rendezvous operation sequencing.关键词
航天器/交会对接/交会敏感器/交会轨迹Key words
spacecraft/rendezvous and docking/rendezvous sensors/rendezvous trajectories分类
航空航天引用本文复制引用
朱仁璋,王鸿芳,徐宇杰,魏羽良..美国航天器交会技术研究[J].航天器工程,2011,20(5):11-36,26.
