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[국내논문] Modelling and simulation of a closed-loop electrodynamic shaker and test structure model for spacecraft vibration testing

Advances in aircraft and spacecraft science, v.5 no.2, 2018년, pp.205 - 223  

Waimer, Steffen (Siemens Industry Software NV) ,  Manzato, Simone (Siemens Industry Software NV) ,  Peeters, Bart (Siemens Industry Software NV) ,  Wagner, Mark (European Space Agency ESA) ,  Guillaume, Patrick (Acoustics and Vibration Research Group, Vrije Universiteit Brussel)

Abstract AI-Helper 아이콘AI-Helper

During launch a spacecraft is subjected to a variety of dynamical loads transmitted through the launcher to spacecraft interface or air-born transmission excitations in the acoustic pressure field inside the fairing. As a result, spacecraft are tested on ground to ensure and demonstrate the global i...

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참고문헌 (20)

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  2. Appolloni, M., Bureo Dacal, R., Cozzani, A., Knockaert, R. and Thoen, B. (2015), "Multi-degree-offreedom vibration platform with MIMO controller for future spacecraft testing: and application case for virtual shaker testing", Proceedings of the 29th Aerospace Testing Seminar (ATS), Los Angeles, U.S.A., October. 

  3. Bettacchioli, A. (2014), "Simulation of satellite vibration test", Proceedings of the 13th European Conference on Spacecraft Structure, Materials and Environmental Testing (ECSSMET), Brunswick, Germany, April. 

  4. Bettacchioli, A. and Nali, P. (2015), "Common issues in S/C sine vibration testing and a methodology to predict the sine test responses from very low-level run", Proceedings of the 29th Aerospace Testing Seminar (ATS), Los Angeles, U.S.A., October. 

  5. Cauberghe, B. (2004), "Applied frequency-domain system identification in the field of experimental and operational modal analysis", Ph.D. Dissertation, Vrije Universiteit Brussel, Brussels. 

  6. De Klerk, D., Rixen, D.J. and Voormeeren, S.N. (2008), "General framework for dynamic substructuring: History, review, and classification of techniques", AIAA J., 46(5), 1169-1181. 

  7. ECSS (2013), Space Engineering, Spacecraft Mechanical Loads Analysis Handbook, ECSS-E-HB-32-26A, http://ecss.nl/hbs/published-hbs-on-line/active-engineering-handbooks/, European Cooperation for Space Standardization (ECSS), Noordwijk, The Netherlands, February. 

  8. Lang, G.F. and Snyder, D. (2001), Understanding the Physics of Electrodynamic Shaker Performance, Sound and Vibration, October. 

  9. Manzato, S., Bucciarelli, F., Arras, M., Coppotelli, G., Peeters, B. and Carrella, A. (2014), "Validation of a virtual shaker testing approach for improving environmental testing performance", Proceedings of the 26th International Conference on Noise and Vibration Engineering (ISMA), Leuven, Belgium, September. 

  10. Mao, Z. (2016), "Statistical modeling of wavelet-transform-based features in structural health monitoring", Proceedings of the 34th International Modal Analysis Conference (IMAC), Orlando, U.S.A., January. 

  11. Merry, R.J.E. and Steinbuch, M. (2005), "Wavelet theory and applications", Literature Study, Eindhoven University of Technology, Department of Mechanical Engineering, Control Systems Technology Group, Eindhoven, The Netherlands, June. 

  12. McConnell, K.G. and Varoto, P.S. (1995), Vibration Testing: Theory and Practice, 2nd Edition, John Wiley & Sons, New York, U.S.A. 

  13. NASA (2014), Spacecraft Dynamic Environments Testing, NASA-HDBK-7008, https://standards.nasa.gov/nasa-developed-standards, National Aeronautics and Space Administration (NASA), Office of the NASA Chief Engineer, NASA Technical Standards Program, June. 

  14. Peeters, B., Auweraer, H.V.D., Guillaume, P. and Leuridan, J. (2004), "The PolyMAX frequency-domain method: a new standard for modal parameter estimation?", Shock Vibr., 11(3-4), 395-409. 

  15. Ricci, S., Peeters, B., Fetter, R., Boland, D. and Debille, J. (2009), "Virtual shaker testing for predicting and improving vibration test performance", Proceedings of the 27th International Modal Analysis Conference (IMAC), Orlando, U.S.A., February. 

  16. Siemens Industry Software NV (2016a), LMS Test.Lab Environmental, www.siemens.com/plm/lms, Leuven, Belgium. 

  17. Siemens Industry Software NV (2016b), LMS SCADAS III Data Acquisition Front-end, www.siemens.com/plm/lms, Breda, The Netherlands. 

  18. Waimer, S., Manzato, S., Peeters, B., Wagner, M. and Guillaume, P. (2015), "Derivation and implementation of an electrodynamic shaker model for virtual shaker testing based on experimental data", Proceedings of the 29th Aerospace Testing Seminar (ATS), Los Angeles, U.S.A., October. 

  19. Waimer, S., Manzato, S., Peeters, B., Wagner, M. and Guillaume P. (2016a), "A multiphysical modelling approach for virtual shaker testing correlated with experimental test results", Proceedings of the 34th International Modal Analysis Conference (IMAC), Orlando, U.S.A., January. 

  20. Waimer, S., Manzato, S., Peeters, B., Wagner, M. and Guillaume, P. (2016b), "Modelling and experimental validation of a coupled electrodynamic shaker and test structure simulation model", Proceedings of the 27th International Conference on Noise and Vibration Engineering (ISMA), Leuven, Belgium, September. 

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