Nonlinear system identification; Space structure; Test data
Abstract :
[en] The objective of this technical note is to apply the nonlinear system identification techniques described in the technical note "Nonlinearity identification methods: predictive analyses" to the experimental data gathered on the SmallSat spacecraft structure. Guidelines for nonlinear spacecraft testing and identification are also be provided.
Research center :
ESTEC
Disciplines :
Aerospace & aeronautics engineering
Author, co-author :
Noël, Jean-Philippe ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux
Kerschen, Gaëtan ; Université de Liège - ULiège > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux
Language :
English
Title :
Contract 21539/08/NL/SFe - Advancement of mechanical verification methods for non-linear spacecraft: Exploitation of test data
Publication date :
February 2011
Publisher :
ESA (ESTEC), Noordwijk, Netherlands
Number of pages :
42
Name of the research project :
Advancement of Mechanical Verification Methods for Non-linear Spacecraft Structures
