文献
J-GLOBAL ID:201702215244905822
整理番号:17A1216074
微分補正法を用いた2インパルス地球-月移動の設計【Powered by NICT】
Design of two-impulse Earth-Moon transfers using differential correction approach
著者 (4件):
Lv Meibo
(National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwest Polytechnical University, Xi’an, 710072, China)
,
Tan Minghu
(National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwest Polytechnical University, Xi’an, 710072, China)
,
Zhou Daming
(National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwest Polytechnical University, Xi’an, 710072, China)
,
Zhou Daming
(Institut de recherche sur les transports l’energie et la societe (IRTES) - EA 7274, Universite de Technologie de Belfort-Montbeliard, Belfort 90000, France)
資料名:
Aerospace Science and Technology
(Aerospace Science and Technology)
巻:
60
ページ:
183-192
発行年:
2017年
JST資料番号:
W1580A
ISSN:
1270-9638
資料種別:
逐次刊行物 (A)
記事区分:
原著論文
発行国:
オランダ (NLD)
言語:
英語 (EN)