Methods for the vibration determination and parameter identification of spacecraft with flexible structures


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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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