WEKO3
アイテム
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Planning, operation and results of the ALFLEX flight trials
https://jaxa.repo.nii.ac.jp/records/37209
https://jaxa.repo.nii.ac.jp/records/37209a5dad5f7-c293-4d16-bfef-db125ae875af
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0039006.pdf (6.0 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Planning, operation and results of the ALFLEX flight trials | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ALFLEX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小型自動着陸実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヘリコプター飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 懸吊飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE型小型実験機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低速飛行特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 自動着陸システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空力学特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2打上げ型有翼回収機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | VTOL | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 垂直離着陸機 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ALFLEX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Automatic Landing Flight Experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | helicopter flight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hanging flight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE shaped vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low speed flying characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | automatic landing system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H 2 Orbiting Plane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | VTOL | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vertical takeoff and landing | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル | ||||||
その他のタイトル | ALFLEX飛行試験の立案、実施および結果 | |||||
著者 |
藤井, 謙司
× 藤井, 謙司× 田中, 敬司× 岡田, 典秋× 中安, 英彦× 辻本, 隆× 土本, 圭司× 吉桑, 栄二× 久司, 一博× Fujii, Kenji× Tanaka, Keiji× Okada, Noriaki× Nakayasu, Hidehiko× Tsujimoto, Takashi× Tsuchimoto, Keiji× Yoshikuwa, Eiji× Hisaji, Kazuhiro |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory 巻 39T, p. 59-72, 発行日 1998-08 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 航空宇宙技術研究所 宇宙開発事業団 28 Feb. 1997 Sydney | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | National Aerospace Laboratory. National Space Development Agency of Japan 28 Feb. 1997 Sydney Australia | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 1996年7月6日に第1回のALFLEX着陸試験が成功し、合計13回の着陸試験が8月15日までに終了した。ALFLEXがユニークであり先例がない特徴を使用しており、その試験が外国で行われたので、計画の最も重大なテーマのうちの1つは、そのような実験のための方法論を確立するということだった。この論文では、飛行試験前や試験中に設定する実験条件、立案、準備、試行日の手続き、試行の方法、コミュニケーション・リンクをはじめ、VTOL(垂直離着陸)型ヘリコプターおよび追跡ヘリコプターの操作に関する活動をまとめて要約する。さらに、飛行試験の結果を説明する。ALFLEX飛行試験では計画の達成に関する次のような結論が得られた。(1)飛行データは、制御、誘導および航行システムの操作・性能を確認し、無人小型実験機に使用された自動着陸技術が適切であることを確認した。(2)HOPE型の形状を持つ小型実験機の低速飛行特性のデータを集めた。(3)懸吊飛行や最大限に数学的なモデルを含むステップアップ手続きの利用により縮小モデル実験機を組み込む飛行試験方法論を実証することができた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The first ALFLEX (Automatic Landing Flight Experiment) landing trial was conducted on July 6, 1996 with success and 13 landing trials in total were completed by August 15. As the ALFLEX has employed unique and unprecedented features and its trials were conducted in a foreign country, one of the most crucial themes of the program was to establish the methodology for such and experiment. In this paper, activities toward and during the flight test such as setting the experiment conditions, planning, preparation, the procedure on the trial day, the method of the trials, communications links, as well as operation of the VTOL (Vertical Takeoff and Landing) helicopter and the chase helicopter are summarized. Also, the outcome of the flight trials is explained. Conclusions of the ALFLEX flight trials are given with regard to the goals of the program as: (1) the flight data confirmed performance of the control, guidance and navigation system, and thereby established that the automatic landing technology used for this type of unmanned vehicle is appropriate; (2) data of the low speed flying characteristics of the vehicle having a shape of the HOPE were collected; and (3) flight test methodology incorporating a scaled model vehicle by utilizing a stepping up procedure including hanging flights and mathematical models to the full extent has been demonstrated. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001565006 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-39T |