文献
J-GLOBAL ID:201702277392048841
整理番号:17A1649060
打上ロケットのためのファジィ適応姿勢コントローラの設計【Powered by NICT】
Fuzzy adaptive attitude controller design for launch vehicle
著者 (4件):
Pei Wang
(College of Astronautics, Northwestern Polytechnical University, National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi’an, China)
,
Bo Lv Mei
(College of Astronautics, Northwestern Polytechnical University, National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi’an, China)
,
Lei Ge Zhi
(College of Astronautics, Northwestern Polytechnical University, National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi’an, China)
,
Shan Xu
(College of Astronautics, Northwestern Polytechnical University, National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi’an, China)
資料名:
IEEE Conference Proceedings
(IEEE Conference Proceedings)
巻:
2017
号:
ICRAS
ページ:
58-63
発行年:
2017年
JST資料番号:
W2441A
資料種別:
会議録 (C)
記事区分:
原著論文
発行国:
アメリカ合衆国 (USA)
言語:
英語 (EN)