Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | Computational Methods in Stochastic Dynamics |
| Herausgeber/-innen | Manolis Papadrakakis, George Stefanou, Vissarion Papadopoulos |
| Herausgeber (Verlag) | Springer Netherlands |
| Seiten | 215-235 |
| Seitenumfang | 21 |
| Band | 2 |
| Publikationsstatus | Veröffentlicht - 2013 |
| Extern publiziert | Ja |
Publikationsreihe
| Name | Computational Methods in Applied Sciences |
|---|---|
| ISSN (Print) | 1871-3033 |
| ISSN (elektronisch) | 2543-0203 |
Abstract
The accurate prediction of the structural response of spacecraft systems during launch and ascent phase is a crucial aspect in design and verification stages which requires accurate numerical models. The enhancement of numerical models based on experimental data is denoted model updating and focuses on the improvement of the correlation between finite element (FE) model and test structure. In aerospace industry the examination of the agreement between model and real structure involves the comparison of the modal properties of the structure. Model updating techniques have to handle several difficulties, like incomplete experimental data, measurement errors, non-unique solutions and modeling uncertainties. To cope with the computational challenges associated with the large-scale FE-models involving up to over one million degrees of freedom (DOFs), enhanced strategies are required. A large-scale numerical example, namely a satellite model, will be used for demonstrating the applicability of the employed updating procedure to complex aerospace structures.
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Tief- und Ingenieurbau
- Mathematik (insg.)
- Modellierung und Simulation
- Ingenieurwesen (insg.)
- Biomedizintechnik
- Informatik (insg.)
- Angewandte Informatik
- Chemische Verfahrenstechnik (insg.)
- Fließ- und Transferprozesse von Flüssigkeiten
- Mathematik (insg.)
- Computational Mathematics
- Ingenieurwesen (insg.)
- Elektrotechnik und Elektronik
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- BibTex
- RIS
Computational Methods in Stochastic Dynamics. Hrsg. / Manolis Papadrakakis; George Stefanou; Vissarion Papadopoulos. Band 2 Springer Netherlands, 2013. S. 215-235 (Computational Methods in Applied Sciences).
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Beitrag in Buch/Sammelwerk › Forschung › Peer-Review
}
TY - CHAP
T1 - Efficient Model Updating of the GOCE Satellite Based on Experimental Modal Data
AU - Goller, B.
AU - Broggi, M.
AU - Calvi, A.
AU - Schuëller, G. I.
N1 - Funding Information: This research was partially supported by the European Space Agency (ESA) under Contract No. 20829/07/NL/EM, which is gratefully acknowledged by the authors. The authors thank Thales Alenia Space Italy for the FE-model of the GOCE satellite and the experimental modal data. The first author is a recipient of a DOC-fForte-fellowship of the Austrian Academy of Science at the Institute of Engineering Mechanics (University of Innsbruck).
PY - 2013
Y1 - 2013
N2 - The accurate prediction of the structural response of spacecraft systems during launch and ascent phase is a crucial aspect in design and verification stages which requires accurate numerical models. The enhancement of numerical models based on experimental data is denoted model updating and focuses on the improvement of the correlation between finite element (FE) model and test structure. In aerospace industry the examination of the agreement between model and real structure involves the comparison of the modal properties of the structure. Model updating techniques have to handle several difficulties, like incomplete experimental data, measurement errors, non-unique solutions and modeling uncertainties. To cope with the computational challenges associated with the large-scale FE-models involving up to over one million degrees of freedom (DOFs), enhanced strategies are required. A large-scale numerical example, namely a satellite model, will be used for demonstrating the applicability of the employed updating procedure to complex aerospace structures.
AB - The accurate prediction of the structural response of spacecraft systems during launch and ascent phase is a crucial aspect in design and verification stages which requires accurate numerical models. The enhancement of numerical models based on experimental data is denoted model updating and focuses on the improvement of the correlation between finite element (FE) model and test structure. In aerospace industry the examination of the agreement between model and real structure involves the comparison of the modal properties of the structure. Model updating techniques have to handle several difficulties, like incomplete experimental data, measurement errors, non-unique solutions and modeling uncertainties. To cope with the computational challenges associated with the large-scale FE-models involving up to over one million degrees of freedom (DOFs), enhanced strategies are required. A large-scale numerical example, namely a satellite model, will be used for demonstrating the applicability of the employed updating procedure to complex aerospace structures.
UR - http://www.scopus.com/inward/record.url?scp=84963553940&partnerID=8YFLogxK
U2 - 10.1007/978-94-007-5134-7_13
DO - 10.1007/978-94-007-5134-7_13
M3 - Contribution to book/anthology
AN - SCOPUS:84963553940
VL - 2
T3 - Computational Methods in Applied Sciences
SP - 215
EP - 235
BT - Computational Methods in Stochastic Dynamics
A2 - Papadrakakis, Manolis
A2 - Stefanou, George
A2 - Papadopoulos, Vissarion
PB - Springer Netherlands
ER -