Stabilization Strategy of Delta-V Assisted Periodic Orbits around Asteroids Based on an Augmented Monodromy Matrix
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- KIKUCHI Shota
- Department of Aeronautics and Astronautics, The University of Tokyo
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- TSUDA Yuichi
- Institute of Space and Astronautical Science, JAXA
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- KAWAGUCHI Junichiro
- Institute of Space and Astronautical Science, JAXA
抄録
<p>Motion around small asteroids, given their weak gravity fields, is strongly affected by perturbation forces such as solar radiation pressure. Several types of orbits in such strongly perturbed environment have been proposed in past studies. However, these orbits usually have complex shapes and limited orbital geometries. To avoid these disadvantages, delta-V assisted periodic orbits (DVAPOs), which are made periodic by introducing a small impulsive delta-V within each period, are proposed. Stability analysis of DVAPOs is the main topic of this paper. The stability of DVAPOs can be analyzed by treating delta-V maneuvers as part of the natural motion and extending the conventional stability analysis method for natural periodic orbits. Moreover, the stability of feed-back controlled DVAPOs can also be discussed by introducing an augmented monodromy matrix. Based on an augmented monodromy matrix, stabilization strategies for DVAPOs are successfully established. Finally, the feasibility of a DVAPO for the Hayabusa 2 mission is shown. </p>
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 14 (ists30), Pd_85-Pd_94, 2016
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
- 1390001205319620096
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- NII論文ID
- 130005420808
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- ISSN
- 18840485
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- Crossref
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- KAKEN
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- 抄録ライセンスフラグ
- 使用不可