Trajectory control for a spacecraft with an inflatable braking device in the Martian atmosphere

被引：0
|
作者：
Aleksashkin, SN [1 ]
Bobylev, AV
Vlasenko, OV
Pichkhadze, KM
Terterashvili, AV
Yaroshevsky, VA
机构：
[1] Babakin Res Ctr, Moscow, Russia
[2] Zhukovsky Cent Aerohydrodynam Inst, Zhukovskii, Moscow Oblast, Russia
来源：
COSMIC RESEARCH | 2003年 / 41卷 / 03期
关键词：
Atmosphere; Control Problem; Martian Atmosphere; Trajectory Control; Parking Orbit;
D O I：
10.1023/A:1024011200969
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The possibility of using an inflatable braking device for controlled descent in the Martian atmosphere of large-capacity cargoes is analyzed. The most complicated version of the trajectory control problem is considered, namely, the injection of a spacecraft at hyperbolic velocity into a parking orbit after braking in the atmosphere.
引用
收藏
页码：280 / 284
页数：5
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