文献
J-GLOBAL ID:202002262850440987
整理番号:20A1189973
オートパイロット遅れと入力飽和を考慮した三次元衝突角度制約適応誘導則【JST・京大機械翻訳】
Three-dimensional impact angle-constrained adaptive guidance law considering autopilot lag and input saturation
著者 (12件):
Lin Defu
(School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China)
,
Lin Defu
(Beijing Key Laboratory of UAV Autonomous Control, Beijing Institute of Technology, Beijing, China)
,
Ji Yi
(School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China)
,
Ji Yi
(Beijing Key Laboratory of UAV Autonomous Control, Beijing Institute of Technology, Beijing, China)
,
Wang Wei
(School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China)
,
Wang Wei
(Beijing Key Laboratory of UAV Autonomous Control, Beijing Institute of Technology, Beijing, China)
,
Wang Yuchen
(School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China)
,
Wang Yuchen
(Beijing Key Laboratory of UAV Autonomous Control, Beijing Institute of Technology, Beijing, China)
,
Wang Hui
(School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China)
,
Wang Hui
(Beijing Key Laboratory of UAV Autonomous Control, Beijing Institute of Technology, Beijing, China)
,
Zhang Fubiao
(School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China)
,
Zhang Fubiao
(Beijing Key Laboratory of UAV Autonomous Control, Beijing Institute of Technology, Beijing, China)
資料名:
International Journal of Robust and Nonlinear Control
(International Journal of Robust and Nonlinear Control)
巻:
30
号:
9
ページ:
3653-3671
発行年:
2020年
JST資料番号:
W0520A
ISSN:
1049-8923
CODEN:
IJRCEA
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)