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Comparative Study on Trajectory Optimization for Solar Sail Mercury Mission
http://hdl.handle.net/10228/0002001101
http://hdl.handle.net/10228/0002001101a117e3eb-8129-4c71-84e7-9ed07f07c948
| 名前 / ファイル | ライセンス | アクション |
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10444303.pdf (929 KB)
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| アイテムタイプ | 会議発表論文 = Conference Paper(1) | |||||||||||||
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| 公開日 | 2025-01-10 | |||||||||||||
| 資源タイプ | ||||||||||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||||||||||
| 資源タイプ | conference paper | |||||||||||||
| タイトル | ||||||||||||||
| タイトル | Comparative Study on Trajectory Optimization for Solar Sail Mercury Mission | |||||||||||||
| 言語 | en | |||||||||||||
| 言語 | ||||||||||||||
| 言語 | eng | |||||||||||||
| 著者 |
Esit, Mehmet
× Esit, Mehmet
× Barros, Leticia
× 平木, 講儒
WEKO
228
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| 抄録 | ||||||||||||||
| 内容記述タイプ | Abstract | |||||||||||||
| 内容記述 | Solar sailing is considered one of the most promising interplanetary spacecraft mission technologies as it does not require any type of conventional propellant. The solar sail attached to the spacecraft allows the use of solar radiation pressure as a continuous low-thrust propulsion system, propelling the spacecraft to travel throughout the solar system. This study focuses on optimizing the trajectory of solar sails for missions to Mercury using the shooting method, a trajectory optimization technique. A comparative analysis is conducted to examine the differences in designing orbital transfers between Mars and Mercury for solar sail missions. The study also compares the performance of current and near-future cubesat solar sails using the performance measures obtained from the literature. Furthermore, the study considers different launch options in the presence of hyperbolic excess velocity obtained from the launch vehicle. The results emphasize the greater sensitivity of the Mars mission to launch window considerations due to its longer orbital time, whereas the Mercury mission offers more flexibility. Increasing the hyperbolic excess velocity significantly reduces the transfer time for Mercury missions, highlighting its importance. The results also show that varying the lightness ratio from current cubesat solar sails to the potential near-future solar sails had a significant impact on the transfer time and trajectory of the missions. Overall, the study provides valuable insights into optimizing cubesats solar sail trajectories for interplanetary missions. | |||||||||||||
| 言語 | en | |||||||||||||
| 備考 | ||||||||||||||
| 内容記述タイプ | Other | |||||||||||||
| 内容記述 | 34th International Symposium on Space Technology and Science, The 34th ISTS, June 3-9, 2023, Kurume, Fukuoka, Japan | |||||||||||||
| 言語 | en | |||||||||||||
| 書誌情報 |
発行日 2023-06 |
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| 会議記述 | ||||||||||||||
| 会議名 | International Symposium on Space Technology and Science | |||||||||||||
| 回次 | 34 | |||||||||||||
| 開始年 | 2023 | |||||||||||||
| 開始月 | 6 | |||||||||||||
| 開始日 | 3 | |||||||||||||
| 終了年 | 2023 | |||||||||||||
| 終了月 | 6 | |||||||||||||
| 終了日 | 9 | |||||||||||||
| 開催国 | JPN | |||||||||||||
| 出版タイプ | ||||||||||||||
| 出版タイプ | VoR | |||||||||||||
| 出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||||||||||
| 査読の有無 | ||||||||||||||
| 値 | no | |||||||||||||
| 研究者情報 | ||||||||||||||
| URL | https://hyokadb02.jimu.kyutech.ac.jp/html/19_ja.html | |||||||||||||
| 論文ID（連携） | ||||||||||||||
| 値 | 10444303 | |||||||||||||
| 連携ID | ||||||||||||||
| 値 | 12642 | |||||||||||||
