文献
J-GLOBAL ID:201802249691752542
整理番号:18A1508808
最大相関Kalmanフィルタに基づく弾道ミサイルのためのSINS/CNS統合航法システム【JST・京大機械翻訳】
SINS/CNS Integrated Navigation System for Ballistic Missile based on Maximum Correntropy Kalman Filter
著者 (7件):
Hou Bowen
(National University of Defense Technology, Department of Mathematics and System Science, CO, 410072, P.R.China)
,
He Zhangming
(National University of Defense Technology, Department of Mathematics and System Science, CO, 410072, P.R.China)
,
Zhou Haiyin
(National University of Defense Technology, Department of Mathematics and System Science, CO, 410072, P.R.China)
,
Zhou Xuanying
(National University of Defense Technology, Department of Mathematics and System Science, CO, 410072, P.R.China)
,
Sun Bowen
(National University of Defense Technology, Department of Mathematics and System Science, CO, 410072, P.R.China)
,
Xu Shuqing
(National University of Defense Technology, Department of Mathematics and System Science, CO, 410072, P.R.China)
,
Wang Jiongqi
(National University of Defense Technology, Department of Mathematics and System Science, CO, 410072, P.R.China)
資料名:
IEEE Conference Proceedings
(IEEE Conference Proceedings)
巻:
2018
号:
ACC
ページ:
1473-1478
発行年:
2018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)