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A Free-Flight Support System
https://jaxa.repo.nii.ac.jp/records/34456
https://jaxa.repo.nii.ac.jp/records/3445619e92090-e8e2-426b-87ed-7a3ff05c4dca
名前 / ファイル | ライセンス | アクション |
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SA2400852.pdf (2.5 MB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | A Free-Flight Support System | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
著者 |
AZUMA, Akira
× AZUMA, Akira× TOMITA, Bunji× IUCHI, Matsusaburo× MISHIMA, Hideo× IWATA, Tadami× KOMOTO, Akira |
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著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
Shimadzu Seisakusho Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Shimadzu Seisakusho Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Shimadzu Seisakusho Ltd. | ||||||
出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Aeronautical Science,University of Tokyo | |||||
書誌情報 |
en : ISAS report/Institute of Space and Aeronautical Science,University of Tokyo 巻 37, 号 3, p. 71-104, 発行日 1972-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This is the second part of the report titled "A New Running Test Facility for the Study of Flight Dynamics" [1]. A support system for free flight of a model aircraft simulated to V/STOL plane or helicopter has been constructed as an additional equipment for the running test facility. The support system is consisted of a free-flight follower and a data reduction system. The free-flight follower can be carried on a carriage moving on a track and supports the model as it can fly either freely or in partly constrained freedom. The flight path and attitude angles of the model during flight can be sensed with potentiometers on the support system and recorded in oscillograms or stored in memories of a miniature computer through an A-D converter, a part of or all of which are boarded on the carriage as the data reduction system. By analyzing the data the aero and/or flight dynamic characteristics of the model will be obtained. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0372-1418 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00675986 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA2400852000 |