書誌事項
- タイトル別名
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- Design of Stiffness and Damping Allocation for Spacecraft Docking Mechanism through 2-DOFs Model
抄録
<p>Docking of spacecraft is an essential technology for various space missions, including building large space structures and resupplying space stations. The docking mechanism has three critical functions: guiding, latching, and damping. Functions after docking such as permanent fixation are outside of this paper’s scope. Three functions mentioned above determine the required minimum and allowable maximum docking speed. This study proposes a new approach to design the stiffness and damping allocation in the docking mechanisms using a 2-DOFs spring-mass model focusing on the energy transfer. To demonstrate the design, we conducted experiments to compare the results with the analytical ones from the viewpoints of the lower limit docking speed, maximum impact force, and maximum displacement of the damper. The experimental results showed that our approach is useful for designing docking mechanisms.</p>
収録刊行物
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- Dynamics & Design Conference
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Dynamics & Design Conference 2023 (0), 601-, 2023
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390580793844643968
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- ISSN
- 24242993
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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
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- 抄録ライセンスフラグ
- 使用不可