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小型無人機の衝突安全の研究
https://jaxa.repo.nii.ac.jp/records/1979
https://jaxa.repo.nii.ac.jp/records/1979c78a5d78-9a69-40c1-8a25-0425eb36e4f0
名前 / ファイル | ライセンス | アクション |
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62246000.pdf (6.9 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 小型無人機の衝突安全の研究 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Collision safety research for a small UAV against human | |||||
著者 |
平林, 大輔
× 平林, 大輔× 石川, 和敏× 金子, 宣彦× 村山, 勉× Hirabayashi, Daisuke× Ishikawa, Kazutoshi× Kaneko, Nobuhiko× Murayama, Tsutomu |
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著者所属 | ||||||
宇宙航空研究開発機構航空プログラムグループ無人航空機利用技術チーム(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空プログラムグループ無人航空機利用技術チーム(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
UAS Applications Technology Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
UAS Applications Technology Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発報告 en : JAXA Research and Development Report 巻 JAXA-RR-13-002, p. 1-42, 発行日 2014-02-28 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本論文は小型無人機(MTOW 数kg までのものに限定する)の利用拡大を可能とする安全基準を策定するために,対人衝突の影響を調査したものである.小型無人機の衝突安全の基準化はこれまでにない初めての試みであり,対人影響として既に存在している一般工業製品の安全基準を参考に小型無人機の衝突安全評価方法を検討した.そして人体ダミーと小型無人機の衝突実験を計画し,実験とFEM 解析の整合性を評価した.以上に基づき小型無人機の衝撃吸収構造の衝突安全性評価方法とその設計技術について提案するものである. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents collision effect of a small UAV nose (MTOW within few kg) against a human head in order to establish safety standards for the purpose of the enhancement of a small UAV utilization. The evaluation method of a small UAV’s collision safety is studied with reference to public industrial products which already have safety standards, because the standardization of the collision safety for a small UAV is the unprecedented first trial. Based on the studies, the experimental methods of a small UAV’s collision are established and FEM analyses are also carried out to compare with the experimental results. As the result, theevaluation method of the collision safety and the design method of the shock absorption structures are proposed. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0062246000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-13-002 |