Enviar artigo por via de e-mail Methods for the vibration determination and parameter identification of spacecraft with flexible structures
- Autores: Ivanov D.S.1, Meus S.V.2, Ovchinnikov A.V.2, Ovchinnikov M.Y.1, Shestakov S.A.1, Yakimov E.N.2
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Afiliações:
- Institute of Applied Mathematics
- AO Information Satellite Systems
- Edição: Volume 56, Nº 2 (2017)
- Páginas: 311-327
- Seção: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219866
- DOI: https://doi.org/10.1134/S1064230717010087
- ID: 219866
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Resumo
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.
Sobre autores
D. Ivanov
Institute of Applied Mathematics
Autor responsável pela correspondência
Email: danilivanovs@gmail.com
Rússia, Moscow
S. Meus
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Rússia, Zheleznogorsk
A. Ovchinnikov
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Rússia, Zheleznogorsk
M. Ovchinnikov
Institute of Applied Mathematics
Email: danilivanovs@gmail.com
Rússia, Moscow
S. Shestakov
Institute of Applied Mathematics
Email: danilivanovs@gmail.com
Rússia, Moscow
E. Yakimov
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Rússia, Zheleznogorsk
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