Attitude control of spinning solar sails based on modal analysis

Yuki Takao, Shota Kikuchi, Osamu Mori, Jun’ichiro Kawaguchi

研究成果: Conference contribution

抄録

Attitude dynamics and control of spinning solar sails are investigated considering the flexibility of sail membranes. Attitude maneuver of solar sails is, in many cases, performed using thrusters. In most studies, the attitude motion is analyzed assuming that the spacecraft is a rigid disk. However, the sail membrane deforms during attitude maneuver due to flexibility. This may cause coupled vibration between the spacecraft main body and sail membrane. This study presents an analysis model of spinning solar sail attitude dynamics considering sail deformation, based on modal analysis.

本文言語English
ホスト出版物のタイトルAAS/AIAA Astrodynamics Specialist Conference, 2018
編集者Puneet Singla, Ryan M. Weisman, Belinda G. Marchand, Brandon A. Jones
出版社Univelt Inc.
ページ2825-2834
ページ数10
ISBN(印刷版)9780877036579
出版ステータスPublished - 2018
外部発表はい
イベントAAS/AIAA Astrodynamics Specialist Conference, 2018 - Snowbird, United States
継続期間: 2018 8 192018 8 23

出版物シリーズ

名前Advances in the Astronautical Sciences
167
ISSN(印刷版)0065-3438

Conference

ConferenceAAS/AIAA Astrodynamics Specialist Conference, 2018
国/地域United States
CitySnowbird
Period18/8/1918/8/23

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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