JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
62246000.pdf6.73 MB
Other TitleCollision safety research for a small UAV against human
Author(jpn)平林, 大輔; 石川, 和敏; 金子, 宣彦; 村山, 勉
Author(eng)Hirabayashi, Daisuke; Ishikawa, Kazutoshi; Kaneko, Nobuhiko; Murayama, Tsutomu
Author Affiliation(jpn)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); 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); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA)
Author Affiliation(eng)UAS Applications Technology Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA); UAS Applications Technology Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA)
Issue Date2014-02-28
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構研究開発報告
JAXA Research and Development Report
Start page1
End page42
Publication date2014-02-28
Abstract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.
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.
Description形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Document TypeTechnical Report
JAXA Category研究開発報告
NASA Subject CategoryAircraft Design, Testing and Performance
Report NoJAXA-RR-13-002

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