Email this article Methods for the vibration determination and parameter identification of spacecraft with flexible structures
- Authors: 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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Affiliations:
- Institute of Applied Mathematics
- AO Information Satellite Systems
- Issue: Vol 56, No 2 (2017)
- Pages: 311-327
- Section: 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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Abstract
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.
About the authors
D. S. Ivanov
Institute of Applied Mathematics
Author for correspondence.
Email: danilivanovs@gmail.com
Russian Federation, Moscow
S. V. Meus
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Russian Federation, Zheleznogorsk
A. V. Ovchinnikov
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Russian Federation, Zheleznogorsk
M. Yu. Ovchinnikov
Institute of Applied Mathematics
Email: danilivanovs@gmail.com
Russian Federation, Moscow
S. A. Shestakov
Institute of Applied Mathematics
Email: danilivanovs@gmail.com
Russian Federation, Moscow
E. N. Yakimov
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Russian Federation, Zheleznogorsk
