書誌事項
- タイトル別名
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- Two-dimensional Response Analysis of Lunar/Planetary Spacecraft by Means of Base-extension Separation Landing Mechanism
- シンキコキ ブンリ チャクリク キコウ オ モチイタ ツキ ワクセイ タンサキ ノ 2ジゲン オウトウ カイセキ
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説明
Next-generation lunar/planetary exploration spacecraft need to solve problems of conventional landing methods and mechanisms such as high rebound, impossibility of reuse and high cost. For this purpose, the authors discuss the landing method by means of Base-Extension Separation landing Mechanism (BESM) which uses energy conversion with springs and separable units. In conventional studies, its effectiveness was confirmed for a simple case based on single-axis restriction. However, the investigation of tumble prevention cannot be treated in the simple case. The purpose of this paper is the response analysis with a double-axis case and to discuss the robustness of BESM for more practical landing situations.
収録刊行物
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- 計測自動制御学会論文集
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計測自動制御学会論文集 51 (7), 515-517, 2015
公益社団法人 計測自動制御学会
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詳細情報 詳細情報について
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- CRID
- 1390001204509863808
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- NII論文ID
- 130005092298
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- NII書誌ID
- AN00072392
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- ISSN
- 18838189
- 04534654
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- NDL書誌ID
- 026618411
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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
- NDL
- Crossref
- CiNii Articles
- KAKEN
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- 抄録ライセンスフラグ
- 使用不可
