文献
J-GLOBAL ID:201802279955294952
整理番号:18A0160488
アクチュエータ故障とモデル不確実性を持つ極超音速滑空機の適応多変数積分TSMC【Powered by NICT】
Adaptive Multivariable Integral TSMC of a Hypersonic Gliding Vehicle With Actuator Faults and Model Uncertainties
著者 (4件):
Li Peng
(College of Mechatronics Engineering and Automation, State Key Laboratory of High Performance Computing, National University of Defense Technology, Changsha, China)
,
Yu Xiang
(Department of Mechanical, Industrial, and Aerospace Engineering, Concordia University, Montreal, QC, Canada)
,
Zhang Youmin
(Department of Mechanical, Industrial, and Aerospace Engineering, Concordia University, Montreal, QC, Canada)
,
Peng Xiaoyan
(College of Mechanical and Vehicle Engineering, Hunan University, Changsha, China)
資料名:
IEEE/ASME Transactions on Mechatronics
(IEEE/ASME Transactions on Mechatronics)
巻:
22
号:
6
ページ:
2723-2735
発行年:
2017年
JST資料番号:
W0894A
ISSN:
1083-4435
CODEN:
IATEFW
資料種別:
逐次刊行物 (A)
記事区分:
原著論文
発行国:
アメリカ合衆国 (USA)
言語:
英語 (EN)