OPTIMIZATION OF THE LUNAR TRANS-EARTH INJECTION WITH THE MULTI-IMPULSE TRANSFER

被引：0

作者：

Gavrikova, Nadezhda M. ^{[1
,2
]}

机构：

[1] Fed State Unitary Enterprise Mars Moscow Expt Des, 16,1 St Shemilovskiy Lane, Moscow 127473, Russia

[2] Lomonosov Moscow State Univ, Dept Theoret Mech & Mechatron, Fac Mech & Math, GSP-1,1 Leninskiye Gory,Main Bldg, Moscow 119991, Russia

来源：

THIRD IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2017 | 2017年 / 161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 problem of the return from the Moon's artificial satellite orbit to the Earth is considered. The main goal is to develop and to implement the algorithm for the lunar trans-Earth injection's trajectory computation using three impulse maneuvers. The advantage of using the trajectory of multi-impulse transfer is that the total costs of the characteristic velocity in this case are less than the one-impulse transfer. Different schemes of the impulse maneuvers sequence are compared. The results of the numerical simulation for the three-body problem (the Earth, the Moon, the spacecraft) considering noncentral gravity models are presented.

引用

页码：627 / 638

页数：12

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