Identifying parameter-dependent volterra kernels to predict aeroelastic instabilities

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

Volumn 1, Issue , 2004, Pages 151-164

  Lind, Rick ^a,d   Prazenica, Richard J ^b,d   Brenner, Martin J ^b,e   Baldelli, Dario H ^c,d  

^a UNIVERSITY OF FLORIDA   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^c ZONA Technology   (United States)

^d 231 Aerospace Building ^*  (United States)

^e Aerostructures Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DAMPING; DATA REDUCTION; FLIGHT DYNAMICS; IDENTIFICATION (CONTROL SYSTEMS); MATHEMATICAL MODELS; NATURAL FREQUENCIES; STIFFNESS MATRIX; VECTORS;

AEROELASTIC SYSTEMS; FLIGHT TESTING; PITCH-PLUNGE SYTEM; VOLTERRA KERNELS;

AERODYNAMICS;

EID: 16244404613     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-1517     Document Type: Conference Paper

References (12)

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4. Lind, R., "Match-Point Solutions for Robust Flutter Analysis," Journal of Aircraft, Vol. 39, No. 1, January-February 2002, pp. 91-99.
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6. Lind, R., Prazenica, R.J. and Brenner, M.J., "Estimating Nonlinearity using Volterra Kernels in Feedback with Linear Models," AIAA-2003-1406, April 2003.
7. Mortagua, J.P. and Lind, R., "Accurate Flutterometer Predictions using Volterra Modeling with Modal Parameter Estimation," 2003-1405, April 2003.
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10. Rugh, W.J., Nonlinear System Theory: The Volterra-Wiener Approach, John Wiley & Sons, 1980.
11. Schetzen, M., The Volterra and Wiener Theories of Nonlinear Systems, John Wiley & Sons, 1980.
12. Silva, W., "Application of Nonlinear Systems Theory to Transonic Unsteady Aerodynamic Responses," Journal of Aircraft, Vol. 30, No. 5, 1993, pp. 660-668.