書誌事項
- タイトル別名
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- Pseudo Periodic Orbit Around an Asteroid in a Circular Orbit
- 公開日
- 2019
- DOI
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- 10.2322/astj.jsass-d-18-00026
- 公開者
- 一般社団法人 日本航空宇宙学会
この論文をさがす
説明
<p>This study discusses a pseudo periodic orbit that is a nearly periodic orbit around a small asteroid such as the Martian moon Deimos. By taking differences of orbital elements between the spacecraft and the asteroid as state variables, basic equations of the relative motion are derived based on Gauss' variational equations. From the basic equations, the initial state of the spacecraft to fly on the pseudo periodic orbit and its period are approximately derived. Furthermore, the stability of the pseudo periodic orbit is analytically examined from the state transition matrix of the linearized equation around the nominal orbit. Numerical studies are executed to verify the analytical results of the conditions and stability of the pseudo periodic orbit.</p>
収録刊行物
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- 航空宇宙技術
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航空宇宙技術 18 (0), 47-56, 2019
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282763100650752
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- NII論文ID
- 130007604457
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- ISSN
- 18840477
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可
