Estimation of solar radiation pressure parameters for solar sail demonstrator ikaros considering attitude dynamics

Yuya Mimasu, Jozef C. Van Der Ha, Tomohiro Yamaguchi, Ryu Funase, Yuichi Tsuda, Osamu Mori, Jun'ichiro Kawaguchi

研究成果: Conference contribution

5 被引用数 (Scopus)

抄録

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 IKAROS 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.

本文言語English
ホスト出版物のタイトルSpaceflight Mechanics 2010 - Advances in the Astronautical Sciences
ホスト出版物のサブタイトルProceedings of the AAS/AIAA Space Flight Mechanics Meeting
ページ1915-1932
ページ数18
出版ステータスPublished - 2010
外部発表はい
イベントAAS/AIAA Space Flight Mechanics Meeting - San Diego, CA, United States
継続期間: 2010 2 142010 2 17

出版物シリーズ

名前Advances in the Astronautical Sciences
136
ISSN(印刷版)0065-3438

Conference

ConferenceAAS/AIAA Space Flight Mechanics Meeting
国/地域United States
CitySan Diego, CA
Period10/2/1410/2/17

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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