Estimates of FRFs from output-only data of a space mission payload component

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 5, Issue , 2006, Pages 3628-3639

  Coppotelli, G ^a,b,c   Balis Crema, L ^a,b  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

^b Dipartimento di Ingegneria Aerospaziale e Astronautica   (Italy)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ELECTRONS; FUNCTION EVALUATION; LAUNCHING; MODAL ANALYSIS; PARAMETER ESTIMATION; TELESCOPES;

ENERGY PHENOMENA; LARGE AREA TELESCOPE (LAT); TRAY STRUCTURES;

SPACE RESEARCH;

EID: 34147136137     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-1887     Document Type: Conference Paper

References (18)

1. GLAST website - http://www-glast.stanford.edu/mission.html
2. L., Balis Crema, G., Coppotelli, Structural Damage Identification from Frequency Response Function Estimates in Proc. of IFASD 2005, June 28 - July 01, Munich, D, (2005).
3. G. Coppotelli, P. Marzocca, A. Behal, Structural Health Monitoring Techniques for Aerospace Applications, in Proc. of 46th AIAA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics, and Material Conference, Austin, TX, USA, paper n. AIAA-2005-2227, (2005).
4. G. Coppotelli, R. Di Conza, F. Mastroddi, R. Pascual, M.A. Caponero, Damage Identification in Composite Plates by Dynamic Displacement Measurements, in Proc. of 2004 International Modal Analysis Seminar, KU Leuven, Belgium, pp. 417-432, (2004).
5. G. Coppotelli, L., Balis Crema, Quality Control of Space Mission Composite Elements by Dynamic Measurements, to be published in Rivista Italiana di Compositi e Nanotecnologie, Materiali, Aerospazio, Tecnologie Speciali, Vol. 1, No. 1, Apr., 2006.
6. R. Pascual, J.C. Golinval, M. Razeto, A Frequency Domain Correlation Technique for Model Correlation and Updating, in XV International Modal Analysis Conference, Orlando, FL, USA, (1997), pp. 587-592
7. th IMAC, S. Antonio, TX, (USA), (2000).
8. P. Van Overschee, B. De Moor Subspace Identification for Linear Systems, Kluver Academic Publisher, (1996).
9. A. Agneni, L. Balis Crema, G. Coppotelli, Time and Frequency Domain Model Parameter Estimation by Output Only Functions, in Proc. of International Forum on Aeroelasticity and Structural Dynamics, Amsterdam, NL, (2003).
10. G. De Vries, Sondage des Systemes Vibrantes par Masses Additionelles, La Recherche Aeronatique, No. 30, Paris, pp. 47-49, (1952).
11. J. Deweer, B. Dierckx, Obtaining Scaled Modal Model of Panel Type Structures Using Acoustic Excitation, XVII IMAC, pp. 2042-2048, (1999).
12. R. Brinker, P. Andersen, A Way of Getting Scaled Mode Shapes in Output Only Modal Testing, in Proceedings of XXI International Modal Analysis Conference, Kissimmee, FL, USA, pp. 141-145, (2003).
13. G. Coppotelli, Identification of Frequency Response Functions by "Output-Only" Experimental Data, in Proceedings of XVII Associazione Italiana di Aeronautica e Astronautica, Rome, ITALY, (2003).
14. L. Balis Crema, G. Coppotelli, Output-Only Approach for Finite Element Model Updating of AB-204 Helicopter Blade, in Proc. of 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Material Conference, Austin, TX, USA, paper n. AIAA-2005-2249, (2005).
15. G. Coppotelli, F. Mastroddi, Output-Only Analysis On Aeroelastic Systems, accepted for the publication and presentation of XVII Associazione Italiana di Aeronautica e Astronautica Conference, Volterra - Pisa, ITALY, 19-22/Sept., (2005).
16. J. Lardies, Modal Parameter Identification from Output-Only Measurements, Mechanics Research Communications, Vol. 24, No. 5, pp. 521-528, (1997).
17. st IMAC, pp. 41-46, (2003).
18. H. Van der Auweraer, L. Hermans, B. Dierckx, J. Deweer In-Operational Modal Analysis: Theory and Application, Course on Modal Analysis: Theory and Practice ISMA 25, 11-12,Sept. (2000)