JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
48461000.pdf37.8 MB
title再突入宇宙機の軌道と誘導
Other TitleOrbit and guidance of reentry spacecraft
Author(jpn)田中 俊輔
Author(eng)Tanaka, Shunsuke
Author Affiliation(jpn)宇宙航空研究開発機構
Author Affiliation(eng)Japan Aerospace Exploration Agency
Issue Date2005-03-25
PublisherJapan Aerospace Exploration Agency (JAXA)
宇宙航空研究開発機構
Publication date2005-03-25
Languagejpn
DescriptionJAXA Research and Development Report
宇宙航空研究開発機構研究開発報告
Keywordsorbit calculation; reentry trajectory; Kepler law; guidance; recoverable spacecraft; atmospheric entry; trajectory control; equation of motion; ballistic trajectory; lift force; aerodynamic drag; spacecraft control; oscillation; neighboring optimum method; closed form equation; 軌道計算; 再突入軌道; ケプラーの法則; 誘導; 再利用宇宙機; 大気圏突入; 軌道制御; 運動方程式; 弾道軌道; 揚力; 空力学的抗力; 宇宙船制御; 振動; 近接最適化法; クローズドフォーム方程式
Document TypeTechnical Report
JAXA Category研究開発報告
ISSN1349-1113
SHI-NOAA0048461000
Report NoJAXA-RR-04-056
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/31040


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.