JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
65046000.pdf1.54 MB
title回転翼機用フライト・シミュレータにおけるモーション・システムの設定
Other TitleMotion System Setup for Rotorcraft Flight Simulator
Author(jpn)萩原, 敏正; 舩引, 浩平; 若色, 薫
Author(eng)Hagiwara, Toshimasa; Funabiki, Kohei; Wakairo, Kaoru
Author Affiliation(jpn)宇宙航空研究開発機構研究開発本部飛行技術研究センター飛行シミュレーションセクション; 宇宙航空研究開発機構研究開発本部飛行技術研究センター飛行シミュレーションセクション; 宇宙航空研究開発機構研究開発本部飛行技術研究センター飛行シミュレーションセクション
Author Affiliation(eng)Flight Simulation Section, Flight Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA); Flight Simulation Section, Flight Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA); Flight Simulation Section, Flight Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Issue Date2011-09-30
Publisher宇宙航空研究開発機構
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構研究開発報告
JAXA research and development report
VolumeJAXA-RR-11-002
Start page1
End page10
Publication date2011-09-30
Languagejpn
eng
AbstractThe previous studies have confirmed that the phase margin in Pilot-in-the-loop shows objective motion system setup adequacy based on an assumption that the phase margin will be increased according to the improved motion cue which affects pilot estimation. || In this study, first, heave and yaw phase margins of JAXA rotorcraft flight simulator were measured varying motion system setup, because it assumed they are typically different from airplane flight simulator. Next, the adequacy of motion system setups resulted from phase margin measurements was verified by the pilot comments through stop and go tasks, side step tasks, etc. And it was also confirmed whether these motion system setups should be reflected in other motion system setups. Finally, all motion system setups of JAXA rotorcraft flight simulator became adequate.
本研究では,JAXA 回転翼機用シミュレータのモーション・システムを最適化することを目的とし,回転翼機と固定翼機で大きく異なると想定されるHeave(上下)とYaw 方向の位相余有をモーション・システムの設定を変えながら測定した. || また,Heave とYaw の位相余有の測定で得られたモーション・システムのフィルタの時定数等の設定の可否を判断し,その設定をHeave とYaw 以外の軸の設定に反映すべきかどうかを判断するためにシミュレータによる確認フライトを実施し,パイロット・コメントより全設定の最適値を求めた.
DescriptionPhysical characteristics: Original contains color illustrations
形態: カラー図版あり
KeywordsRotorcraft Flight Simulator; Motion; System; Setup; Evaluation; Handling Quality; Phase Margin
Document TypeTechnical Report
JAXA Category研究開発報告
ISSN1349-1113
NCIDAA1192675X
SHI-NOAA0065046000
Report NoJAXA-RR-11-002
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/14318


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