Spacecraft Formation Flying in Eccentric Orbits
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- Yamada Katsuhiko
- 名古屋大学大学院工学研究科
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- Shima Takeya
- 三菱電機(株)先端技術総合研究所
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- Jikuya Ichiro
- 名古屋大学大学院工学研究科
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- Yoshikawa Shoji
- 三菱電機(株)先端技術総合研究所
Bibliographic Information
- Other Title
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- 楕円軌道のフォーメーションフライトに関する考察
- ダエン キドウ ノ フォーメーション フライト ニ カンスル コウサツ
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Abstract
Formation flight of spacecraft in eccentric orbits is considered in this paper. Symmetry of the eccentric orbits is assumed in a relative formation orbit, and under this assumption, relations of initial conditions in formation flight are derived. Some characteristic orbits are obtained from these relations, such as an orbit where a deputy spacecraft rotates around a chief spacecraft with relatively small variation in the distance between the two spacecraft, or an orbit where the deputy spacecraft moves on a local horizontal plane on which the chief spacecraft exists. Formation flight by plural spacecraft is possible by combining these relative orbits.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 56 (650), 97-104, 2008
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282679445307648
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- NII Article ID
- 10021152944
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 9419963
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed