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Yves Govers
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Stochastic model updating—Covariance matrix adjustment from uncertain experimental modal data
Y Govers, M Link
Mechanical systems and signal processing 24 (3), 696-706, 2010
1272010
Sensitivity or Bayesian model updating: a comparison of techniques using the DLR AIRMOD test data
E Patelli, Y Govers, M Broggi, HM Gomes, M Link, JE Mottershead
Archive of Applied Mechanics 87, 905-925, 2017
842017
A multivariate interval approach for inverse uncertainty quantification with limited experimental data
M Faes, M Broggi, E Patelli, Y Govers, J Mottershead, M Beer, D Moens
Mechanical Systems and Signal Processing 118, 534-548, 2019
782019
A review of experimental modal analysis methods with respect to their applicability to test data of large aircraft structures
M Boeswald, D Goege, U Fuellekrug, Y Govers
Proc. of the international conference on noise and vibration engineering …, 2006
662006
A comparison of two stochastic model updating methods using the DLR AIRMOD test structure
Y Govers, HH Khodaparast, M Link, JE Mottershead
Mechanical Systems and Signal Processing 52, 105-114, 2015
572015
Analysis of sources and quantification of uncertainty in experimental modal data
Y Govers, M Böswald, U Füllekrug, D Göge, M Link
Proceedings of the International Seminar on Modal Analysis, 4161-4173, 2006
362006
Online monitoring of aircraft modal parameters during flight test based on permanent output-only modal analysis
G Jelicic, J Schwochow, Y Govers, J Sinske, R Buchbach, J Springer
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2017
322017
Measurement of FRFs and modal identification in case of correlated multi‐point excitation
U Füllekrug, M Böswald, D Göge, Y Govers
Shock and Vibration 15 (3-4), 435-445, 2008
312008
Fuzzy finite element model updating of the DLR AIRMOD test structure
HH Khodaparast, Y Govers, I Dayyani, S Adhikari, M Link, MI Friswell, ...
Applied Mathematical Modelling 52, 512-526, 2017
292017
Airbus a350 xwb gvt: state-of-the-art techniques to perform a faster and better GVT Campaign
P Lubrina, S Giclais, C Stephan, M Boeswald, Y Govers, N Botargues
Topics in Modal Analysis II, Volume 8: Proceedings of the 32nd IMAC, A …, 2014
272014
Comparison of Bayesian and interval uncertainty quantification: Application to the AIRMOD test structure
M Broggi, M Faes, E Patelli, Y Govers, D Moens, M Beer
2017 IEEE Symposium Series on Computational Intelligence (SSCI), 1-8, 2017
262017
System identification and tracking using a statistical model and a Kalman filter
K Soal, Y Govers, J Bienert, A Bekker
Mechanical Systems and Signal Processing 133, 106127, 2019
222019
New concepts for ground and flight vibration testing of aircraft based on output-only modal analysis
M Böswald, J Schwochow, G Jelicic, Y Govers
Proceedings of the 7th International Operational Modal Analysis Conference …, 2017
212017
Taxi vibration testing-An alternative method to ground vibration testing of large aircraft
M Böswald, Y Govers
International Conference on Noise and Vibration Engineering (ISMA2008), 2008
212008
AIRBUS A350XWB Ground Vibration Testing: Efficient techniques for customer oriented on-site modal identification
Y Govers, M Böswald, P Lubrina, S Giclais, C Stephan, N Botargues
Proceedings of the International Conference on Noise and Vibration …, 2014
172014
Experimental and operational modal analysis: Automated system identification for safety-critical applications
R Volkmar, K Soal, Y Govers, M Böswald
Mechanical Systems and Signal Processing 183, 109658, 2023
162023
Optimization & testing of aeroelastically-tailored forward swept wings
MY Meddaikar, J Dillinger, MR Ritter, Y Govers
162017
Parameter identification of structural dynamic models by inverse statistical analysis
Y Govers
152012
New excitation signals for aircraft ground vibration testing
S Giclais, P Lubrina, C Stéphan, M Böswald, Y Govers, J Ufer, ...
Proceedings" IFASD 2011", 2011
142011
Solar Impulse–How to validate the numerical model of a superlight aircraft with A340 dimensions
M Böswald, Y Govers, A Vollan, M Basien
Proceedings of ISMA 2010, 2451, 2010
142010
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