JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
62065000.pdf14.84 MB
title小型飛行船型無人機の研究開発
Other TitleResearch & Develop program of the Small Airship type UAV
Author(jpn)河野, 敬; 奥山, 政広; 都甲, 章己; 中舘, 正顯; 松田, 幸雄
Author(eng)Kohno, Takashi; Okuyama, Masahiro; Togou, Shouki; Nakadate, Masaaki; Matsuda, Yukio
Author Affiliation(jpn)宇宙航空研究開発機構航空本部運航システム・安全技術研究グループ; 宇宙航空研究開発機構航空本部航空技術実証研究開発室; 宇宙航空研究開発機構; 宇宙航空研究開発機構航空本部運航システム・安全技術研究グループ; 宇宙航空研究開発機構航空本部運航システム・安全技術研究グループ
Author Affiliation(eng)Operation Systems and Safety Technology Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA); Technology Demonstration Research Office, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Operation Systems and Safety Technology Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA); Operation Systems and Safety Technology Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)
Issue Date2013-11-30
Publisher宇宙航空研究開発機構(JAXA)
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
VolumeJAXA-RR-13-004
Start page1
End page161
Publication date2013-11-30
Languagejpn
eng
Abstract災害監視等に供する無人機システムとして,飛行船型無人機システムの研究開発を実施した.災害時に迅速かつ容易に運用できる飛行船型無人機を実現するために必要な技術として,飛行誘導制御技術と運用技術に着目した.それぞれについて研究開発を実施し,個別の試験機による飛行試験により技術実証をおこなった.飛行誘導制御技術については自動制御飛行が可能な14m 級の飛行船型無人機を開発し,2007-2008 年度に飛行試験をおこなった.また,運用技術については専用地上装置を用いた先進的な地上運用技術を取り入れた小型電動飛行船を開発し,2009年度に飛行試験をおこなったほか,地方自治体による防災訓練に参加するなどのデモンストレーションを実施した.更に,確立されたそれら技術を用いた,災害監視用のプロトタイプとなる12m 級飛行船型無人機試験機の試作をおこなった.
R&D on unmanned aerial vehicle (UAV) systems for the disaster monitoring has been conducted at JAXA since 2005. The Airship type UAV is expected to be the essential part of such disaster monitoring UAVsystem. In order to develop the Airship UAV that can be useful in the actual disaster scene, flight controltechnology and operation technology are considered to be necessary. Two experimental vehicles were developed to prove each technology. 14m class Airship UAV was able to conduct automatic flight includinghovering and simulated take off and landing. The flight test was conducted in 2007 and 2008. A new method of the ground handling including inflation and deflation of the envelope of the airship was developed. An small electric-driven remotely controlled airship (9m class) was developed with the devised ground handling system. The flight test was conducted in 2009 and a demonstration flight in the disaster exercise by the local government was also conducted. Finally, 12m class Airship UAV was developed as a prototype of the disaster monitoring airship UAV with flight control technology and operation technology that are proven by the flight tests using the preceding two experimental vehicles.
Description形態: 図版あり
Physical characteristics: Original contains illustrations
KeywordsAirship; UAV; Flight Control; Operation; Flight Test
Document TypeTechnical Report
JAXA Category研究開発報告
NASA Subject CategoryAircraft Design, Testing and Performance
ISSN1349-1113
NCIDAA1192675X
SHI-NOAA0062065000
Report NoJAXA-RR-13-004
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/22064


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