書誌事項
- タイトル別名
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- Optimal Trajectory of Powered Descending Phase with Coasting for Smart Lander for Investigating Moon
抄録
<p>This paper is on optimal trajectory of future lunar lander with coasting in powered descending phase. For the light weight/low cost lunar lander, optical navigation using onboard cameras to identify their current state is one of very few techniques available to achieve the pin-point landing. The optical navigation is to be operated between the powered descending phases, when the orbital maneuvering engine (OME) is turned off. This paper shows the series of different coasting conditions and discusses the effect of the coasting to the trajectory and fuel consumption. The results give some ideas for future gravitational planetary missions, which uses coasting during their powered descending phase. In addition, optimal trajectory with double coasting for the SLIM project is shown in this paper.</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 17 (0), 55-60, 2018
一般社団法人 日本航空宇宙学会
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詳細情報
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- CRID
- 1390282680296469504
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- NII論文ID
- 130006639021
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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