Methods for the vibration determination and parameter identification of spacecraft with flexible structures
- 作者: Ivanov D.1, Meus S.2, Ovchinnikov A.2, Ovchinnikov M.1, Shestakov S.1, Yakimov E.2
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隶属关系:
- Institute of Applied Mathematics
- AO Information Satellite Systems
- 期: 卷 56, 编号 2 (2017)
- 页面: 311-327
- 栏目: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219866
- DOI: https://doi.org/10.1134/S1064230717010087
- ID: 219866
如何引用文章
详细
Methods for dynamic parameters identification and vibrations estimation of large spacecraft with flexible structures are reviewed. Different approaches to the structural deviation determination and to the vibration frequency identification by processing measurements from the onboard sensors are compared. Measuring devices and sensors for the motion estimation of large nonrigid structures are reviewed.
作者简介
D. Ivanov
Institute of Applied Mathematics
编辑信件的主要联系方式.
Email: danilivanovs@gmail.com
俄罗斯联邦, Moscow
S. Meus
AO Information Satellite Systems
Email: danilivanovs@gmail.com
俄罗斯联邦, Zheleznogorsk
A. Ovchinnikov
AO Information Satellite Systems
Email: danilivanovs@gmail.com
俄罗斯联邦, Zheleznogorsk
M. Ovchinnikov
Institute of Applied Mathematics
Email: danilivanovs@gmail.com
俄罗斯联邦, Moscow
S. Shestakov
Institute of Applied Mathematics
Email: danilivanovs@gmail.com
俄罗斯联邦, Moscow
E. Yakimov
AO Information Satellite Systems
Email: danilivanovs@gmail.com
俄罗斯联邦, Zheleznogorsk
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