THE TRAJECTORY CONTROL STRATEGIES OF AKATSUKI FOR VENUS ORBIT REINSERTION

被引：0

作者：

Hirose, Chikako ^{[1
]}

Ishii, Nobuaki ^{[1
]}

Kawakatsu, Yasuhiro ^{[1
]}

Ukai, Chiaki ^{[2
]}

Terada, Hiroshi ^{[2
]}

机构：

[1] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Chuou Ku, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 2525210, Japan

[2] NEC Aerosp Syst Ltd, Fuchu, Tokyo 1838501, Japan

来源：

SPACEFLIGHT MECHANICS 2013, PTS I-IV | 2013年 / 148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 Japanese Venus explorer "Akatsuki (PLANET-C)", which now rotates about the Sun, will approach to Venus again in 2015. For the Venus orbit reinsertion, several trajectory strategies were devised. In this paper, we introduce the difficulties we faced in redesigning the trajectory of Akatsuki after the failure of the first Venus Orbit Insertion (VOI) in 2010 and report some newly devised trajectory control strategies including Gravity Brake Method, which will make the most of the solar perturbations to conduct the Venus orbit insertion for the second time.

引用

页码：2909 / 2918

页数：10

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