QQ客服 官方微博 反馈留言

	Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method
	Li, Xiongfei; Cheng, Wei
刊名	INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING
	2018
卷号	2018
关键词	Computational efficiency Degrees of freedom (mechanics) Dynamic response Flexible spacecraft Frequency response MATLAB Connection interface Control moment gyroscope Degrees of freedom (DoFs) Dynamic substructure Frequency response functions Multibody dynamics simulations Prediction accuracy Spacecraft structures Gyroscopes
ISSN号	1687-5966
DOI	10.1155/2018/5045740
URL标识	查看原文
收录类别	SCIE ; EI
WOS记录号	WOS:000430680000001
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5933176
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Li, Xiongfei,Cheng, Wei. Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method[J]. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING,2018,2018.
APA	Li, Xiongfei,&Cheng, Wei.(2018).Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method.INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING,2018.
MLA	Li, Xiongfei,et al."Research on Microvibrations Generated by a Control Moment Gyroscope on a Flexible Interface Based on a Dynamic Substructure Method".INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING 2018(2018).

个性服务

查看访问统计

相关权益政策

暂无数据

收藏/分享

除非特别说明，本系统中所有内容都受版权保护，并保留所有权利。