Interplanetary trajectory design of solar sail spacecraft utilizing an invariant manifold

Yutaro Ishida, Shinji Hokamoto

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

抄録

This paper deals with an in-plane trajectory design method for a solar sail spacecraft to rendezvous with a planet. In the interplanetary rendezvous problem, the spacecraft's velocity must coincide with the orbital velocity of the planet when it reaches the planet's orbit. This paper proposes a trajectory design procedure that utilizes an invariant manifold for a specified control profile to reach a target orbit. The proposed strategy allows a rendezvous to a planet in an elliptical orbit by adjusting the launch timing of the sailcraft when it starts from a circular orbit. Numerical simulations demonstrate the validity of the proposed procedure.

本文言語英語
ホスト出版物のタイトルAIAA/AAS Astrodynamics Specialist Conference 2010
DOI
出版ステータス出版済み - 12 1 2010
イベントAIAA/AAS Astrodynamics Specialist Conference 2010 - Toronto, ON, カナダ
継続期間: 8 2 20108 5 2010

出版物シリーズ

名前AIAA/AAS Astrodynamics Specialist Conference 2010

その他

その他AIAA/AAS Astrodynamics Specialist Conference 2010
国/地域カナダ
CityToronto, ON
Period8/2/108/5/10

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • エネルギー(全般)

フィンガープリント

「Interplanetary trajectory design of solar sail spacecraft utilizing an invariant manifold」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

引用スタイル