Active vibration control of flexible appendages of spacecraft during attitude maneuver | |
Wang, Zelin; Zhou, Wenya; Wang, Xiaoming | |
2018 | |
会议名称 | 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018 |
会议日期 | 2018-10-01 |
会议地点 | Bremen, Germany |
会议录 | 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018
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URL标识 | 查看原文 |
WOS记录号 | [DB:DC_IDENTIFIER_WOSID] |
内容类型 | 会议论文 |
URI标识 | http://www.corc.org.cn/handle/1471x/3235115 |
专题 | 大连理工大学 |
作者单位 | 1.Dalian University of Technology, Dalian, 116024, China 2.State Key Laboratory of Structural Analysis for Industrial Equipment, School of Aeronautics and Astronautics, Dalian University of Technology, Dalian, 116024, China 3.School of Aeronautics and Astronautics, Sun Yat-sen University, Guangzhou, 510006, China |
推荐引用方式 GB/T 7714 | Wang, Zelin,Zhou, Wenya,Wang, Xiaoming. Active vibration control of flexible appendages of spacecraft during attitude maneuver[C]. 见:69th International Astronautical Congress: #InvolvingEveryone, IAC 2018. Bremen, Germany. 2018-10-01. |
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