<b>The Transfer Orbit to Moon in the Planar Restricted Elliptic </b><b>Three-Body Problems</b>
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- Onozaki Kaori
- Major in Applied Mechanics, Waseda University
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- Yoshimura Hiroaki
- Major in Applied Mechanics, Waseda University
Bibliographic Information
- Other Title
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- 平面楕円制限<b>3</b>体問題における月への輸送軌道の設計
- 平面楕円制限3体問題における月への輸送軌道の設計
- ヘイメン ダエン セイゲン 3タイ モンダイ ニ オケル ツキ エ ノ ユソウ キドウ ノ セッケイ
- The Transfer Orbit to Moon in the Planar Restricted Elliptic Three-Body Problems
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Abstract
For the design of spacecraft transfer orbits in the Earth-Moon system, we need to model the dynamics in the context of the Planar Elliptic Restricted Three-Body Problem (PER3BP) since it has a non-negligible eccentricity. In this paper, we investigate invariant manifolds of the PER3BP by analyzing Lagrangian Coherent Structures (LCS). In particular, we show that the transfer orbits from the exterior realm to Moon can be developed by employing the geometric characteristics of the LCS obtained by long time numerical integrations.
Journal
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- Transactions of the Institute of Systems, Control and Information Engineers
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Transactions of the Institute of Systems, Control and Information Engineers 27 (4), 160-165, 2014
THE INSTITUTE OF SYSTEMS, CONTROL AND INFORMATION ENGINEERS (ISCIE)
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Keywords
Details 詳細情報について
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- CRID
- 1390282680142597504
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- NII Article ID
- 130004565054
- 40020039938
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- NII Book ID
- AN1013280X
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- ISSN
- 2185811X
- 13425668
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- NDL BIB ID
- 025398886
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
- KAKEN
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- Abstract License Flag
- Disallowed
