Data and model uncertainties in complex aerospace engineering systems

被引:43
作者
Capiez-Lernout, E.
Pellissetti, M.
Pradwarter, H.
Schueller, G. I.
Soize, C.
机构
[1] Univ Marne La Vallee, Lab Mecan, F-77455 Marne La Vallee, France
[2] Leopold Franzens Univ, Inst Engn Mech, A-6020 Innsbruck, Austria
关键词
COMPUTATIONAL STOCHASTIC MECHANICS; RANDOM EIGENVALUE PROBLEMS; NONHOMOGENEOUS UNCERTAINTIES;
D O I
10.1016/j.jsv.2006.01.056
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Parametric probabilistic approaches allow data uncertainties to be modelled, but have some difficulties to represent model uncertainties. It has been recently shown that both model and data uncertainties can be taken into account with a non-parametric approach. Moreover, it is known that with increasing complexity of a mechanical system, model uncertainties also increase. Based on these considerations, both parametric and non-parametric probabilistic approaches are used on a complex system of aerospace engineering constituted of a satellite coupled with its launcher. First, a parametric probabilistic model is constructed for analysing the sensitivity of the response due to data uncertainties. Then, the non-parametric probabilistic model is introduced with the same uncertainty level in order to study the sensitivity of the response with respect to the model and the data uncertainties. The dynamical responses obtained with these two probabilistic approaches are analysed in order to quantify the sensitivity of the structure to data uncertainties as well as model uncertainties. (c) 2006 Elsevier Ltd. All rights reserved.
引用
收藏
页码:923 / 938
页数:16
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