ORBIT DETERMINATION ANALYSIS OF VENUS SPACE PROBE "AKATSUKI (PLANET-C)"

被引：0
|
作者：
Ichikawa, Tsutomu [1 ]
Ishii, Nobuaki [1 ]
Hirose, Chikako [1 ]
Takeuchi, Hiroshi [1 ]
Taniguchi, Sho [2 ]
Yagami, Tomoko [2 ]
Ohnishi, Takafumi [2 ]
机构：
[1] Japan Aerosp Explorat Agcy JAXA, Chuo Ku, 3-1-1 Yoshinodai, Kanagawa 2525210, Japan
[2] Fujitsu Ltd, Chiyoda Ku, 3-10 Higashikanda 2, Tokyo 1010031, Japan
来源：
SPACEFLIGHT MECHANICS 2017, PTS I - IV | 2017年 / 160卷
关键词：
D O I：
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中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
First Japanese probe orbiting Venus known as "AKATSUKI (Planet-C)", has been launched on May 21, 2010 on H-IIA booster from Tanegashima Space Center (TSC), Kagoshima, Japan. It arrived at Venus on December 7, 2010, but due to a malfunction of the thruster system, the Venus orbit insertion failed. Using the reaction control systems instead of the broken orbital maneuvering engine, the recovery maneuver was operated on December 7, 2015, and AKATSUKI was finally inserted into an orbit around Venus with a 0.36 million km apoapsis and a 10.5 day. It is described the strategy, analysis, and evaluation for the orbit determination to orbit Venus.
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页码：3355 / 3366
页数：12
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