文献
J-GLOBAL ID:201702269251175621
整理番号:17A1353369
火星同軸回転翼機のホバー性能を評価するための実験装置の設計【Powered by NICT】
Design of experimental setups for evaluating hover performance of a Martian coaxial rotorcraft
著者 (7件):
Zhao Pengyue
(State Key Laboratory of Robotics and System, Harbin Institute of Technology, 150001, Heilongjiang, China)
,
Zhao Zhijun
(State Key Laboratory of Robotics and System, Harbin Institute of Technology, 150001, Heilongjiang, China)
,
Chen Shuitian
(State Key Laboratory of Robotics and System, Harbin Institute of Technology, 150001, Heilongjiang, China)
,
Quan Qiquan
(State Key Laboratory of Robotics and System, Harbin Institute of Technology, 150001, Heilongjiang, China)
,
Li He
(State Key Laboratory of Robotics and System, Harbin Institute of Technology, 150001, Heilongjiang, China)
,
Bai Deen
(State Key Laboratory of Robotics and System, Harbin Institute of Technology, 150001, Heilongjiang, China)
,
Deng Zongquan
(State Key Laboratory of Robotics and System, Harbin Institute of Technology, 150001, Heilongjiang, China)
資料名:
IEEE Conference Proceedings
(IEEE Conference Proceedings)
巻:
2017
号:
ICMA
ページ:
1427-1432
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)