JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
48058000.pdf7.88 MB
Other TitleGuidance and control law design for High Speed Flight Demonstration Phase 2
Author(jpn)塚本 太郎; 鈴木 広一; 二宮 哲次郎
Author(eng)Tsukamoto, Taro; Suzuki, Hirokazu; Ninomiya, Tetsujiro
Author Affiliation(jpn)宇宙航空研究開発機構 総合技術研究本部; 宇宙航空研究開発機構 総合技術研究本部; 宇宙航空研究開発機構 総合技術研究本部
Author Affiliation(eng)Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics; Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics; Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Issue Date2004-10-29
PublisherJapan Aerospace Exploration Agency (JAXA)
Publication date2004-10-29
AbstractThe High-Speed Flight Demonstration Phase 2 is a flight experiment program to investigate the transonic aerodynamic characteristics of the HOPE-X winged re-entry vehicle. A vehicle based on a scaled HOPE-X configuration is lifted by stratospheric balloon to an altitude of 20 to 30-km, from where it will be released into free-fall and accelerate to transonic speeds. To acquire useful aerodynamic data, the guidance and control system must maintain the vehicle's Mach number at a constant value while varying its angle of attack quasi-statically. After data acquisition, the vehicle must be guided to a selected recovery point and attain suitable recovery parameters. In this paper, the design of a guidance and control law to achieve these requirements is described.
DescriptionJAXA Research and Development Report
Keywordshigh speed flight demonstration; winged reentry vehicle; guidance; control; aerodynamic characteristic; transonic flight; angle of attack; balloon; 高速飛行実証; 有翼再突入機; 誘導; 制御; 空力特性; 遷音速飛行; 仰角; 気球
Document TypeTechnical Report
JAXA Category研究開発報告
Report NoJAXA-RR-04-006

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