文献
J-GLOBAL ID:201702291292282190
整理番号:17A1508760
ミサイルオートパイロットのタイムラグの視角制約会計の末端線を用いた規定された性能迎撃ミサイル誘導【Powered by NICT】
Prescribed performance interceptor guidance with terminal line of sight angle constraint accounting for missile autopilot lag
著者 (6件):
Lyu Shi
(School of Astronautics, Northwestern Polytechnical University, Xi’an, 710072, People’s Republic of China)
,
Lyu Shi
(National Key Laboratory of Aerospace Flight Dynamics, Xi’an, 710072, People’s Republic of China)
,
Yan Xiaodong
(School of Astronautics, Northwestern Polytechnical University, Xi’an, 710072, People’s Republic of China)
,
Yan Xiaodong
(National Key Laboratory of Aerospace Flight Dynamics, Xi’an, 710072, People’s Republic of China)
,
Tang Shuo
(School of Astronautics, Northwestern Polytechnical University, Xi’an, 710072, People’s Republic of China)
,
Tang Shuo
(National Key Laboratory of Aerospace Flight Dynamics, Xi’an, 710072, People’s Republic of China)
資料名:
Aerospace Science and Technology
(Aerospace Science and Technology)
巻:
69
ページ:
171-180
発行年:
2017年
JST資料番号:
W1580A
ISSN:
1270-9638
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)