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Assessment of nonlinear system identification methods using the SmallSat spacecraft structure
Kerschen, Gaëtan; Soula, L.; Vergniaud, J.B. et al.
2011In Proceedings of the 29th International Modal Analysis Conference
 

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Abstract :
[en] In this paper, several techniques for nonlinear system identification are applied to a real-world structure, the SmallSat spacecraft structure developed by EADS-Astrium. This composite structure comprises two vibration isolation systems, one of which possesses mechanical stops. The loading case considered in the present study is a random (local) excitation. A careful progression through the different steps of the system identification process, namely detection, characterization and parameter estimation, is carried out. Different methods are applied to data resulting from numerical experiments, without having access to the finite element model which generated these data.
Disciplines :
Aerospace & aeronautics engineering
Author, co-author :
Kerschen, Gaëtan  ;  Université de Liège - ULiège > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux
Soula, L.
Vergniaud, J.B.
Newerla, A.
Language :
English
Title :
Assessment of nonlinear system identification methods using the SmallSat spacecraft structure
Publication date :
2011
Event name :
29th International Modal Analysis Conference
Event place :
Jacksonville, United States
Event date :
February 2011
Audience :
International
Main work title :
Proceedings of the 29th International Modal Analysis Conference
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