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Volumn 1, Issue , 2007, Pages 12-31

Robust flutter prediction for data-based aeroelastic LPV models

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; AIRCRAFT; APPLICATION PROGRAMS; FLIGHT DYNAMICS; SOFTWARE TESTING; WIND TUNNELS; ALGORITHMS; COMPUTATIONAL EFFICIENCY; PARAMETER ESTIMATION; WINGS;

EID: 40549090547     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (12)

References (13)
  • 1
    • 0141947742 scopus 로고
    • A historical overview of flight flutter testing
    • October
    • Kehoe, M.W., "A Historical Overview of Flight Flutter Testing," NASA TM-4720, October 1995.
    • (1995) NASA TM-4720
    • Kehoe, M.W.1
  • 2
    • 85007688839 scopus 로고
    • Prediction of flutter onset speed based on flight testing at subcritical speeds
    • Zimmerman, N. H., Weissenburger, J. T., "Prediction of Flutter Onset Speed Based on flight Testing at Subcritical Speeds," Journal of Aircraft, Vol. 1, No. 4, 1964, pp. 190-202.
    • (1964) Journal of Aircraft , vol.1 , Issue.4 , pp. 190-202
    • Zimmerman, N.H.1    Weissenburger, J.T.2
  • 4
    • 29544445182 scopus 로고    scopus 로고
    • Identifying parameter-dependent volterra kernels to predict aeroelastic instabilities
    • November-December
    • Lind, R., and Prazenica., R. J., Brenner, M. J., and Baldelli, D. H., "Identifying Parameter-Dependent Volterra Kernels to Predict Aeroelastic Instabilities," AIAA Journal, Vol. 42, No. 6, November-December 2005, pp. 2496-2502.
    • (2005) AIAA Journal , vol.42 , Issue.6 , pp. 2496-2502
    • Lind, R.1    Prazenica, R.J.2    Brenner, M.J.3    Baldelli, D.H.4
  • 5
    • 26244465119 scopus 로고    scopus 로고
    • Nonlinear aeroelastic/aeroservoelastic modeling update by block-oriented identification
    • September-October
    • Baldelli, D.H., Lind, R., and Brenner, M., "Nonlinear Aeroelastic/Aeroservoelastic Modeling Update by Block-Oriented Identification," Journal of Guidance, Control, & Dynamics, Vol. 28, No. 5, September-October 2005, pp. 1056-1064.
    • (2005) Journal of Guidance, Control, & Dynamics , vol.28 , Issue.5 , pp. 1056-1064
    • Baldelli, D.H.1    Lind, R.2    Brenner, M.3
  • 6
    • 0036178635 scopus 로고    scopus 로고
    • Match-point solutions for robust flutter analysis
    • January-February
    • Lind, R., "Match-Point Solutions for Robust Flutter Analysis," Journal of Aircraft, Vol. 39, No. 1, January-February 2002, pp. 91-99.
    • (2002) Journal of Aircraft , vol.39 , Issue.1 , pp. 91-99
    • Lind, R.1
  • 8
    • 51349096662 scopus 로고    scopus 로고
    • A poly-reference implementation of the maximum likelihood complex frequency-domain estimator and some industrial applications
    • Dearborn, USA, January
    • Cauberghe, B., Guillaume, P., Verboven, P., Parloo, E., and Vanlanduit, S., "A Poly-Reference Implementation of the Maximum Likelihood Complex Frequency-Domain Estimator and some Industrial Applications," 22nd International Modal Analysis Conference, Dearborn, USA, January 2004.
    • (2004) 22nd International Modal Analysis Conference
    • Cauberghe, B.1    Guillaume, P.2    Verboven, P.3    Parloo, E.4    Vanlanduit, S.5
  • 9
    • 18144402436 scopus 로고    scopus 로고
    • On the influence of the parameter constraint on the stability of the poles and the discrimination capabilities of the stabilization diagrams
    • Cauberghe, B., Guillaume, P., Verboven, P., Vanlanduit, S. and Parloo, E., "On the Influence of the Parameter Constraint on the Stability of the Poles and the Discrimination Capabilities of the Stabilization Diagrams," Mechanical Systems and Signal Processing, Vol. 19, pp. 989-1014, 2005.
    • (2005) Mechanical Systems and Signal Processing , vol.19 , pp. 989-1014
    • Cauberghe, B.1    Guillaume, P.2    Verboven, P.3    Vanlanduit, S.4    Parloo, E.5
  • 10
    • 0031275376 scopus 로고    scopus 로고
    • Nonlinear control of a prototypical wing section with torsional nonlinearity
    • Ko, J., and Kurdila., A. J., Strganac, T. W., "Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity," Journal of Guidance, Control and Dynamics, Vol. 20, No. 6,1997, pages 1181-1189.
    • (1997) Journal of Guidance, Control and Dynamics , vol.20 , Issue.6 , pp. 1181-1189
    • Ko, J.1    Kurdila, A.J.2    Strganac, T.W.3
  • 11
    • 29344463548 scopus 로고    scopus 로고
    • Aircraft system identification: Theroy and practice
    • Reston, VA
    • Klein, V. and Morelli, E.A., "Aircraft System Identification: Theroy and Practice," AIAA Education Series, Reston, VA, 2006.
    • (2006) AIAA Education Series
    • Klein, V.1    Morelli, E.A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.