DYNAMICS OF A STRONGLY NONLINEAR SPACECRAFT STRUCTURE PART I: EXPERIMENTAL IDENTIFICATION

J.P. Noel, Ludovic Renson, Gaetan Kerschen

Research output: Contribution to conferenceConference Paper

Abstract

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.
Original languageEnglish
Publication statusUnpublished - 2014
EventEuropean Conference on Spacecraft Structures, Materials and Environmental Testing (SSMET) - Braunschweig, Germany
Duration: 1 Apr 20144 Apr 2014

Conference

ConferenceEuropean Conference on Spacecraft Structures, Materials and Environmental Testing (SSMET)
CountryGermany
CityBraunschweig
Period1/04/144/04/14

Fingerprint Dive into the research topics of 'DYNAMICS OF A STRONGLY NONLINEAR SPACECRAFT STRUCTURE PART I: EXPERIMENTAL IDENTIFICATION'. Together they form a unique fingerprint.

Cite this