文献
J-GLOBAL ID:202002270291029697
整理番号:20A0273747
宇宙船バスの柔軟性を考慮した宇宙機の統合制御法【JST・京大機械翻訳】
Integrated control method for spacecraft considering the flexibility of the spacecraft bus
著者 (5件):
Tang Liang
(Research and Development Center, Zhongguancun Nansanjie 16#, Haidian District, Beijing Institute of Control Engineering, 100190, Bejing, People’s Republic of China)
,
Guo Zixi
(Research and Development Center, Zhongguancun Nansanjie 16#, Haidian District, Beijing Institute of Control Engineering, 100190, Bejing, People’s Republic of China)
,
Guan Xin
(Research and Development Center, Zhongguancun Nansanjie 16#, Haidian District, Beijing Institute of Control Engineering, 100190, Bejing, People’s Republic of China)
,
Wang Youyi
(Research and Development Center, Zhongguancun Nansanjie 16#, Haidian District, Beijing Institute of Control Engineering, 100190, Bejing, People’s Republic of China)
,
Zhang Kebei
(Research and Development Center, Zhongguancun Nansanjie 16#, Haidian District, Beijing Institute of Control Engineering, 100190, Bejing, People’s Republic of China)
資料名:
Acta Astronautica
(Acta Astronautica)
巻:
167
ページ:
73-84
発行年:
2020年
JST資料番号:
B0035B
ISSN:
0094-5765
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)