| 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 [Université de Liège - ULg > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux >] | |
Noël, Jean-Philippe [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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