並列タイトル等A Dynamic Model Wind-Tunnel Experiment with Gust Alleviation System
タイトル（掲載誌）航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
一般注記In this paper the results of wind-tunnel experiments of a dynamic model with a gust alleviator are reported. The experiments were planned on the basis of previously reported examinations and experiments. The gust alleviation system was a simple verical acceleration feedback system to the flap and elevator. The originally planned system, in which the elevator control law was to have canceled the quasi steady pitching moment produced by the flap,failed during the experiments. The system that succeeded resulted in an elevator control almost 180 degree oppositely phased to the planned system. This inconsistency was in some degree analytically resolved by describing realistic filter characteristics. The experiments was made in the NAL Gust-Wind-Tunnel,using a heave-and-pitchi free 0.1 dynamically rough-scaled model of a Beech Queen Air. As a whole result,the simple model system adopting micromotor serbos,showed possibilities for an economic dyanamic model wind-tunnel experiment.
資料番号: NALTM0463000
レポート番号: NAL TM-463
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44046&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ