MODELING OF ATTITUDE DYNAMICS FOR MAROS SOLAR SAIL DEMONSTRATOR

被引：0
|
作者：
Tsuda, Yuichi [1 ]
Saiki, Takanao [1 ]
Mimasu, Yuya [2 ]
Funase, Ryu [3 ]
机构：
[1] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Chuo Ku, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 2525210, Japan
[2] Kyushu Univ, Dept Aeronaut & Astronaut, Nishi Ku, Fukuoka 8190395, Japan
[3] Japan Aerosp Explorat Agcy, JAXA Space Explorat Ctr, Chuo Ku, Sagamihara, Kanagawa 2525210, Japan
来源：
SPACEFLIGHT MECHANICS 2011, PTS I-III | 2011年 / 140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：
This paper describes a method of modeling attitude dynamics of spinning solar sail spacecraft under influence of solar radiation pressure (SRP). This method is verified and actually exploited in the operation of Japanese interplanetary solar sail demonstration spacecraft IKAROS. MAROS shows a unique attitude behavior due to strong SRP effect. This paper shows a new attitude model of spinning sail, which is verified by flight data of MAROS. It is also shown that the model proposed in this paper has a direct relation with the Generalized Sail Model.
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页码：147 / +
页数：2
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