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ALFLEX全機振動特性確認試験
https://jaxa.repo.nii.ac.jp/records/40317
https://jaxa.repo.nii.ac.jp/records/403177d60d821-071f-44a2-9c62-e6dd6f30a5b0
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr0001370.pdf (1.8 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ALFLEX全機振動特性確認試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ALFLEX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 自動着陸実験 | |||||
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打上げ型無人有翼宇宙往還機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地上振動試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動的変位計測システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動モード解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 慣性測定装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ピッチレート | |||||
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 | 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 | ground vibration test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dynamic displacement measurement system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vibration mode analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | inertial measurement unit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pitch rate | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Confirmation tests of ALFLEX vibration characteristics | |||||
著者 |
神田, 淳
× 神田, 淳× 外崎, 得雄× 上田, 哲彦× Kanda, Atsushi× Sotozaki, Tokuo× Ueda, Tetsuhiko |
|||||
著者所属 | ||||||
航空宇宙技術研究所 構造研究部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 構造研究部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 構造研究部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Structures Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Structures Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Structures Division | ||||||
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報告 en : Technical Report of National Aerospace Laboratory 巻 1370, p. 1-16, 発行日 1998-12 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | モーダル測定にロボットによる動的変位計測装置を用いてALFLEX(自動着陸実験)全機振動試験を行った。本機体はエレボンまわりの剛性アップの改修が行われており、改修後の全機振動試験は今回が初めてである。また、ハンマーインパクト法により局所的なモーダル測定も行い、飛行実験中に発生したIMU(慣性センサ)ピッチレートの振動問題についても考察を行った。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Ground vibration tests of ALFLEX were carried out by using the Dynamic Displacement Measurement System which enables automatic data acquisition. After structural improvements and flight experiments, vibration characteristics of ALFLEX (Automatic Landing Flight Experiment) were confirmed by ground tests. Modal measurements for local vibrations were also conducted by the hammer impact method. The vibration problem that occurred in the pitch rate of IMU (Inertial Measurement Unit) during the flight experiments was considered. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001677000 | |||||
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 TR-1370 |