2014年
1P2-N03 環境温度駆動型の座屈アクチュエータによる微小重力落下試験用ローバーの跳躍特性評価(宇宙ロボット)
ロボティクス・メカトロニクス講演会講演概要集
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- 巻
- 2014
- 号
- 0
- 開始ページ
- _1P2
- 終了ページ
- N03_1-_1P2-N03_2
- 記述言語
- 日本語
- 掲載種別
- 出版者・発行元
- 一般社団法人 日本機械学会
Asteroid probe Hayabusa 2 is developed by JAXA. Asteroid exploration rovers will be carried by Hayabusa 2. In our research project, we have developed an environmental-temperature-driven buckling actuator with a bimetal thin plate for a hopping mechanism of the rover. In this study, to characterize the hopping capability of the actuator, we conducted microgravity examination in ZARM drop tower. We fabricate a test rover for the microgravity examination with a rapid heating system for actuation in short free-fall time. Although reaction force from baseplate was incomplete in take-off, the rover hopped with a vertical velocity of 3.12 mm/s with 0.035 rad/s rotating rate.
- リンク情報
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- CiNii Articles
- http://ci.nii.ac.jp/naid/110009966806
- CiNii Books
- http://ci.nii.ac.jp/ncid/AA11902933
- ID情報
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- CiNii Articles ID : 110009966806
- CiNii Books ID : AA11902933
- identifiers.cinii_nr_id : 9000309157709