ESTIMATION OF SOLAR RADIATION PRESSURE PARAMETERS FOR SOLAR SAIL DEMONSTRATOR IKAROS CONSIDERING ATTITUDE DYNAMICS

被引：0

作者：

Mimasu, Yuya ^{[1
]}

van der Ha, Jozef C. ^{[1
]}

Yamaguchi, Tomohiro ^{[2
]}

Funase, Ryu ^{[3
]}

Tsuda, Yuichi ^{[3
]}

Mori, Osamu ^{[3
]}

Kawaguchi, Jun'ichiro ^{[3
]}

机构：

[1] Kyushu Univ, Dept Aeronaut & Astronaut, Nishi Ku, Fukuoka 8190395, Japan

[2] Grad Univ Adv Studies, Dept Space & Astronaut Sci, Sagamihara, Kanagawa 2298510, Japan

[3] Japan Aerosp Explorat Agcy, Sagamihara, Kanagawa 2298510, Japan

来源：

SPACEFLIGHT MECHANICS 2010, PTS I-III | 2010年 / 136卷

关键词：

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Japan Aerospace Exploration Agency (JAXA) has developed the small demonstration solar sail spacecraft IKAROS (Interplanetary Kite-craft Accelerated by Radiation of the Sun), which will be launched in mid 2010. The main objective of this spacecraft is to deploy the 20m class sail membrane, and demonstrate the acceleration of a spacecraft by the solar radiation pressure (SRP) by means of that sail. It is important to model the SRP force adequately for the objective of navigation, especially for interplanetary spacecraft. In order to improve the model of the SRP torque induced by the sail membrane, the MAROS project team plans to estimate the SRP torque parameters in orbit. In this paper, we present the approach to obtain the parameters needed for constructing the photon torque model through the analysis of the attitude dynamics.

引用

页码：1915 / +

页数：2

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