@inproceedings{oai:jaxa.repo.nii.ac.jp:00037209,
 author = {藤井, 謙司 and 田中, 敬司 and 岡田, 典秋 and 中安, 英彦 and 辻本, 隆 and 土本, 圭司 and 吉桑, 栄二 and 久司, 一博 and Fujii, Kenji and Tanaka, Keiji and Okada, Noriaki and Nakayasu, Hidehiko and Tsujimoto, Takashi and Tsuchimoto, Keiji and Yoshikuwa, Eiji and Hisaji, Kazuhiro},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Aug},
 note = {航空宇宙技術研究所　宇宙開発事業団 28 Feb. 1997 Sydney, National Aerospace Laboratory. National Space Development Agency of Japan 28 Feb. 1997 Sydney Australia, 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。, 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., 資料番号: AA0001565006, レポート番号: NAL SP-39T},
 pages = {59--72},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {Planning, operation and results of the ALFLEX flight trials},
 volume = {39T},
 year = {1998}
}