Methods for the vibration determination and parameter identification of spacecraft with flexible structures
- Авторлар: Ivanov D.1, Meus S.2, Ovchinnikov A.2, Ovchinnikov M.1, Shestakov S.1, Yakimov E.2
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Мекемелер:
- Institute of Applied Mathematics
- AO Information Satellite Systems
- Шығарылым: Том 56, № 2 (2017)
- Беттер: 311-327
- Бөлім: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219866
- DOI: https://doi.org/10.1134/S1064230717010087
- ID: 219866
Дәйексөз келтіру
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.
Авторлар туралы
D. Ivanov
Institute of Applied Mathematics
Хат алмасуға жауапты Автор.
Email: danilivanovs@gmail.com
Ресей, Moscow
S. Meus
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Ресей, Zheleznogorsk
A. Ovchinnikov
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Ресей, Zheleznogorsk
M. Ovchinnikov
Institute of Applied Mathematics
Email: danilivanovs@gmail.com
Ресей, Moscow
S. Shestakov
Institute of Applied Mathematics
Email: danilivanovs@gmail.com
Ресей, Moscow
E. Yakimov
AO Information Satellite Systems
Email: danilivanovs@gmail.com
Ресей, Zheleznogorsk
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