3 A Somewhat Comprehensive Critique of Experimental Modal Analysis 39 References 1. Load Analysis of Spacecraft and Payloads, NASA-STD-5002 (1996) 2. Independent Structural Loads Analysis. U.S. Air Force Space Command, SMC-S-004 (2008) 3. Kabe, A.M., Sako, B.H.: Structural Dynamics Fundamentals and Advanced Applications, vol. 1 & 2. Academic Press, London (2020) 4. Coppolino, R.N.: The Integrated Test Analysis Process for Structural Dynamic Systems. Morgan & Claypool Publishers, San Rafael (2020) 5. Hunt, D., Adams, W., Bock, T.: Dynamic analysis of structures with friction forces at sliding joints. J. Spacecr. Rockets. 21(2) (1984) 6. Henkel, E.E., Misel, J.E., Frederick, D.H.: A methodology to include static and kinetic friction effects in space shuttle payload transient loads analysis. In: Shuttle Environment and Operations Meeting. AIAA, Washington, DC (1983) 7. A friction methodology for space shuttle/payload transient loads analysis. In: Proc. Shuttle Payload Dynamics Loads Prediction Workshop, JPL-D-1347, vol. 2 (1984) 8. Guyan, R.J.: Reduction of stiffness and mass matrices. AIAA J. 3 , 380–381 (1965) 9. Coppolino, R.: Automated response DOF selection for mapping of experimental normal modes. In: IMAC XVI (1998) 10. Tuttle, R.E., Cole, T.R., Lollock, J.A.: An automated method for identification of efficient measurement degrees-of-freedom for modal survey testing. In: 46th AIAA/ASME/ASCE/AHS/ASC SDM Conference (2005) 11. Bendat, J.S., Piersol, A.G.: Random Data Analysis and Measurement Procedures, 4th edn. Wiley, Hoboken (2010) 12. Bendat, J.S.: Nonlinear Systems Techniques and Applications, 2nd edn. Wiley, New York (1998) 13. Bishop, R.E.D., Gladwell, G.M.L.: An investigation into the theory of resonance testing. Philos. Trans. Royal Soc. Lond. Ser. A. 225 , A-105 5 (1963 ) 14. Brown, D.L., Allemang, R.J.: The modern era of experimental modal analysis. Sound Vib. Mag., 85 (2007) 15. Allemang, R.J., Brown, D.L.: Chapter 21: experimental modal analysis. In: Piersol, A.G., Paez, T.L. (eds.) Harris’ Shock and Vibration Handbook, 6th edn. McGraw-Hill, New York. (2010) 16. Coppolino, R.: Methodologies for Verification and Validation of Space Launch System (SLS) Structural Dynamic Models, vol. 1, NASA CR-2018-219800 (2018) 17. Nelder, J., Mead, R.: A simplex method for function minimization. Comput. J. 7(4), 308–313 (1965) 18. Metropolis, N., Ulam, S.: The Monte Carlo Method. J. Am. Stat. Assoc. 44(247), 335–341 (1949) 19. Zimmerman, D.C., Jorgensen, S.S.F.: Parallel multispecies genetic algorithm for physics and parameter estimation in structural dynamics. AIA AJ . 43 , 2224 (2005) 20. Rayleigh, J.W.S.: The Theory of Sound, 1st American edn. Dover Publications, New York (1945) 21. Caughey, T.K., O’Kelly, M.E.J.: Classical normal modes in damped linear dynamic systems. ASME J. Appl. Mech. 32 , 583–588 (1965) 22. Cremer, L., Heckl, M., Ungar, E.: Structure Borne Sound. Springer-Verlag, New York (1973) 23. Coppolino, R.N.: Structural dynamics modeling–tales of sin and redemption. Sound Vib. Mag. 50(1), 7–11 (2016) 24. Mayes, R., Klenke, S.: The SMAC modal parameter extraction package. In: IMAC XVII (1999) 25. Wilkinson, J.H.: The Algebraic Eigenvalue Problem. Oxford University Press, New York (1965) 26. Coppolino, R.N.: The integrated test-analysis process (2020 challenges). In: IMAC XXXVIII (2020) 27. Coppolino, R.N.: Roadmap to a highly improved modal test process. In: IMACXXXVIII (2020) 28. Ibrahim, S.R., Mikulcik, E.C.: A method for the direct identification of vibration parameters from the free response. Shock Vib. Bull. 47 , 183–196 (1977) 29. Juang, J., Pappa, R.S.: An eigensystem realization algorithm for modal parameter identification and model reduction. J. Guid. Control Dyn. 8 , 620–627 (1985) 30. Brincker, R., Ventura, C.E.: Introduction to Operational Modal Analysis. Wiley, Chichester (2015) 31. Golub, G.H., Reinsch, C.: Singular value decomposition and least squares solutions. Numer. Math. 14 , 403–420 (1970) 32. Miller, K.: Complex linear least squares. SIAM Rev. 15(4), 706–726 (1973)
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