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Development and Flight Verification of Airborne Glideslope Computation/Gust Detection System
https://jaxa.repo.nii.ac.jp/records/45167
https://jaxa.repo.nii.ac.jp/records/4516740539ab1-8209-4a5c-a6ae-357574fdc68d
名前 / ファイル | ライセンス | アクション |
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naltr00908.pdf (1.9 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Development and Flight Verification of Airborne Glideslope Computation/Gust Detection 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_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル | ||||||
その他のタイトル | 基準径路設定/突風検出装置の試作と飛行実験による評価 | |||||
著者 |
小野, 孝次
× 小野, 孝次× 古茂田, 真幸× 川幡, 長勝× 塚野, 雄吉× ONO, Takatsugu× KOMODA, Masaki× KAWAHATA, Nagakatsu× TSUKANO, Yukichi |
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著者所属 | ||||||
航空宇宙技術研究所飛行実験部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所飛行実験部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所飛行実験部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所飛行実験部 | ||||||
著者所属(英) | ||||||
en | ||||||
Flight Research Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Flight Research Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Flight Research Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Flight Research Division, National Aerospace Laboratory(NAL) | ||||||
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 TR-908 巻 908, p. 24, 発行日 1986-06 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An airborne Glideslope Computation/Gust Detection System was developed for supporting flight tests of NAL’s Variable Stability and Response Airplane (VSRA). The system includes a set of Kalman filters to estimate position and inertial velocity and utilizes signals from DME, the pressure altimeter, and accelerometers and gyros. Glideslope and localizer deviations from a preselected nominal flight path having an arbitrarily assigned glideslope angle, are computed and transmitted to ADI and HSI instead of the standard ILS signals. Gust components as differences of inertial and air speeds are also estimated. Based upon flight test data, estimated horizontal inertial speed is compared with that obtained from Doppler Radar, and validity and accuracy of gust estimation are verified by state reconstruction techniques. | |||||
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: NALTR0908000 | |||||
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-908 |