ROSETTA: Optimal manoeuvre planning for multiple swing-by trajectories

被引：0
|
作者：
Schoenmaekers, J
机构：
来源：
12TH INTERNATIONAL SYMPOSIUM ON SPACE FLIGHT DYNAMICS | 1997年 / 403卷
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D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A major task for the ROSETTA mission is the optimal planning of the injection orbit, of the manoeuvres during the interplanetary cruise phase and of the parameters for the swing-by's at Mars and at the Earth. The problem has been solved using linear optimization techniques. The paper explains the essentials of the algorithms which are used. Furthermore, it presents the results for the baseline ROSETTA mission to comet Wirtanen.
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页码：327 / 334
页数：8
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