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

页码：280 / 284

页数：5

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