PRELIMINARY DESIGN OF THE PHASING STRATEGY OF A LUNAR ORBIT RENDEZVOUS MISSION

被引：0
|
作者：
Wang, Zhong-Sheng [1 ,2 ]
Meng, Zhanfeng [1 ]
Gao, Shan [1 ]
Liu, Decheng [1 ]
机构：
[1] China Acad Space Technol, 104 Youyi Rd, Beijing 100094, Peoples R China
[2] Embry Riddle Aeronaut Univ, Coll Engn, Daytona Beach, FL 32114 USA
来源：
ASTRODYNAMICS 2013, PTS I-III | 2014年 / 150卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The preliminary design of the phasing strategy of a lunar orbit rendezvous mission is discussed in this paper. A 4-impulse maneuver scheme is selected as the baseline design to help achieve the basic goal of the phasing stage for the chaser, and an optimal nominal phasing strategy is developed based on tracking access analysis and other considerations. Also discussed are the computation of the lunar surface ascent window and the analysis of the influence of the tracking and orbit control error on the aim point dispersion using Monte Carlo numerical simulations and analytical methods.
引用
收藏
页码：2743 / 2762
页数：20
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