4028 静止衛星のソーラーセイルによる最適遷移軌道(S61-2 宇宙システムの誘導・制御(2),21世紀地球環境革命の機械工学:人・マイクロナノ・エネルギー・環境)

• 松田 郁未

  横国大院

• 畑佐 啓太

  横国大院

• 上野 誠也

  横国大

書誌事項

タイトル別名

• 4028 Optimal Transfer Orbit of a Geostationary Satellite by Solar Sail

抄録

The concepts of solar sail have been proposed for a long time. Solar sail is a propulsion system that changes the sunlight into the thrust of the spaceship. Because solar sail doesn't need fuel consumption and it is very lightweight, it attracts attention widely and some studies have been done. In this study, earth circular trajectories are considered and the number of circulars is used as an independent variable for improving the accuracy of optimization calculation. To be concrete, the issue of the satellite injection into the geostationary orbit is discussed. By using optimal transfer trajectories that maximize semimajor axis in one revolution, a new effective injection method was proposed

収録刊行物

• 年次大会講演論文集

  年次大会講演論文集 2008.5 (0), 377-378, 2008

  一般社団法人 日本機械学会

キーワード

• Solar sail
• Geostationary orbit
• Optimal transfer trajectories
• Semimajor axis

詳細情報

• CRID: 1390001206065182080
• NII論文ID: 110007659217
• DOI: 10.1299/jsmemecjo.2008.5.0_377
• ISSN: 24331325
• Web Site: https://www.jstage.jst.go.jp/article/jsmemecjo/2008.5/0/2008.5_377/_pdf
• 本文言語コード: ja
• データソース種別:
  • JaLC
  • Crossref
  • CiNii Articles
• 抄録ライセンスフラグ: 使用不可