Adaptive Fractional Order Positive Position Feedback for Vibration Control of Vertical Tail

被引：0
|
作者：
Zhang, Jiaxuan [1 ,2 ]
Li, Bin [1 ,2 ]
Niu, Wenchao [3 ]
Li, Kaixiang [2 ,4 ]
机构：
[1] School of Aeronautics, Northwestern Polytechnical University, Shaanxi, Xi'an,710072, China
[2] National Key Laboratory of Strength and Structural Integrity, Shaanxi, Xi'an,710065, China
[3] China Ship Development and Design Center, Hubei, Wuhan,430064, China
[4] Aircraft Strength Research Institute of China, Shaanxi, Xi'an,710065, China
来源：
Binggong Xuebao/Acta Armamentarii | 2024年 / 45卷 / 08期
关键词：
22;
D O I：
10.12382/bgxb.2023.0570
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2542 / 2553
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