Reference : Contract 21539/08/NL/SFe - Advancement of mechanical verification methods for non-linear...
Reports : External report
Engineering, computing & technology : Aerospace & aeronautics engineering
http://hdl.handle.net/2268/115370
Contract 21539/08/NL/SFe - Advancement of mechanical verification methods for non-linear spacecraft: Nonlinearity identification methods: predictive analyses
English
Kerschen, Gaëtan mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux >]
Noël, Jean-Philippe mailto [Université de Liège - ULg > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux >]
Dec-2010
ESA (ESTEC)
50
Noordwijk
The Netherlands
[en] Nonlinear system identification ; Space structure
[en] The objective of this technical note is to explore the applicability of nonlinear system identification techniques to spacecraft structures. To this end, numerical experiments carried out using the finite
element model of the SmallSat spacecraft are used, without, however, having access to the model itself. The constraints imposed by the considered techniques for breadboard testing are also highlighted.
ESTEC
European Space Agency (ESA)
Advancement of Mechanical Verification Methods for Non-linear Spacecraft Structures
http://hdl.handle.net/2268/115370

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