Methods for the vibration determination and parameter identification of spacecraft with flexible structures
- Авторы: Ivanov D.1, Meus S.2, Ovchinnikov A.2, Ovchinnikov M.1, Shestakov S.1, Yakimov E.2
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Учреждения:
- Institute of Applied Mathematics
- AO Information Satellite Systems
- Выпуск: Том 56, № 2 (2017)
- Страницы: 311-327
- Раздел: 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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Аннотация
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.
Об авторах
D. Ivanov
Institute of Applied Mathematics
Автор, ответственный за переписку.
Email: danilivanovs@gmail.com
Россия, Moscow
S. Meus
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Россия, Zheleznogorsk
A. Ovchinnikov
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Россия, Zheleznogorsk
M. Ovchinnikov
Institute of Applied Mathematics
Email: danilivanovs@gmail.com
Россия, Moscow
S. Shestakov
Institute of Applied Mathematics
Email: danilivanovs@gmail.com
Россия, Moscow
E. Yakimov
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Россия, Zheleznogorsk
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