The present paper addresses the identification of a real-life spacecraft structure possessing a strongly nonlinear component with multiple mechanical stops. The complete identification procedure, from nonlinearity detection and characterization to parameter estimation, is carried out based upon experimental sine-sweep data collected during a classical spacecraft qualification campaign.
|Publication status||Unpublished - 2014|
|Event||European Conference on Spacecraft Structures, Materials and Environmental Testing (SSMET) - Braunschweig, Germany|
Duration: 1 Apr 2014 → 4 Apr 2014
|Conference||European Conference on Spacecraft Structures, Materials and Environmental Testing (SSMET)|
|Period||1/04/14 → 4/04/14|