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航天器快捷交会技术分析
引用本文:朱仁璋,王鸿芳,丛云天,李颐黎,余梦伦.航天器快捷交会技术分析[J].载人航天,2014(2):139-145.
作者姓名:朱仁璋  王鸿芳  丛云天  李颐黎  余梦伦
作者单位:[1]北京航空航天大学,北京100191 [2]中国空间技术研究院,北京100094 [3]中国运载火箭技术研究院,北京100076
摘    要:快捷交会对航天乘员与飞行任务都是非常有利的。快捷交会的基本原理是减少调相段飞行圈数;为此,需设计可完成一系列交会程序的较短的飞行时间,并获得与飞行时间相匹配的较小的初相角。快捷交会的关键技术包括提高入轨精度,增强追踪飞行器的自主计算与轨道控制能力,扩大地面站覆盖范围,以及对目标飞行器轨道的精准调整。

关 键 词:交会对接  快捷交会  载人航天  航天器

Analysis on Fast Spacecraft Rendezvous Technology
ZHU Renzhang,WANG Hongfang,CONG Yuntian,LI Yili,YU Menglun.Analysis on Fast Spacecraft Rendezvous Technology[J].Manned spaceflight,2014(2):139-145.
Authors:ZHU Renzhang  WANG Hongfang  CONG Yuntian  LI Yili  YU Menglun
Institution:1. Beihang University, Beijing 100191, China; 2. China Academy of Space Technology, Beijing 100094, China; 3. China Academy of Launch Vehicle Technology, Beijing 100076, China)
Abstract:Fast rendezvous is of benefit to flight crew members and flight tasks .The basic principle is reducing of phasing revolutions .For this, a short rendezvous flight duration , within that a series of rendezvous procedure can be completed , corresponding with the smaller initial phase angle has to be designed .And the key technologies include a precise initial orbit of the chase vehicle , advanced flight control and calculation systems onboard , wide ground control coverage , and the co-ordinated orbital adjustment of the target vehicle .
Keywords:rendezvous and docking  fast rendezvous  human spaceflight  spacecraft
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