| 美国航天器交会技术研究 |
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| 引用本文： | 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. |
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| 作者姓名： | 朱仁璋 王鸿芳 徐宇杰 魏羽良 |
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| 作者单位： | 1. 南京大学,南京,210093
2. 北京航空航天大学,北京,100191 |
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| 摘 要： | 美国交会对接技术的发展可分为三个阶段：＂双子座＂与＂阿波罗＂飞船,航天飞机,以及后航天飞机时代的项目。自主交会技术的发展,首先基于多种制导和导航敏感器的研发,特别是用于最终逼近段的激光敏感器。制导、导航与控制系统的冗余,以及故障检测与隔离的方法,在轨迹安全性中起重要作用。文章研究美国自主交会方案,包括＂双子座＂,＂阿波...
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| 关 键 词： | 航天器 交会对接 交会敏感器 交会轨迹 |
Study on Rendezvous Techniques of American Spacecraft |
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| ZHU Renzhang, WANG Hongfang, XU Yujie WEI Yuliang.Study on Rendezvous Techniques of American Spacecraft[J].Spacecraft Engineering,2011,20(5):11-36. |
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| Authors: | ZHU Renzhang WANG Hongfang XU Yujie WEI Yuliang |
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| Institution: | ZHU Renzhang1,3 WANG Hongfang1,2 XU Yujie3 WEI Yuliang3(1 Nanjing University,Nanjing 210093,China)(2 China Academy of Space Technology,Beijing 100094,China)(3 Beijing University of Aeronautics and Astronautics,Beijing 100191,China) |
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| 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 ... |
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| Keywords: | spacecraft rendezvous and docking rendezvous sensors rendezvous trajectories |
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