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Volumn 3, Issue , 2004, Pages 1691-1704

Robust controller design for active flutter suppression

Author keywords

[No Author keywords available]

Indexed keywords

FLUTTER SUPPRESSION; LINEAR FRACTIONAL TRANSFORMATION (LFT); ROBUST CONTROLLER DESIGN; UNCREWED AERIAL VEHICLES (UAV);

EID: 19944381896     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (15)
  • 1
    • 0141957140 scopus 로고    scopus 로고
    • Historical perspective on analysis and control of aeroelastic responses
    • Mukhopadhyay, V., "Historical Perspective on Analysis and Control of Aeroelastic Responses", Journal of Guidance, Control, and Dynamics Vol. 26, No. 5, 2003, pp. 673-684.
    • (2003) Journal of Guidance, Control, and Dynamics , vol.26 , Issue.5 , pp. 673-684
    • Mukhopadhyay, V.1
  • 2
    • 0032649619 scopus 로고    scopus 로고
    • Gain-scheduled linear fractional control for active flutter suppression
    • Barker, J. M., Balas, G. J. and Blue, P. A., "Gain-Scheduled Linear Fractional Control for Active Flutter Suppression", Journal of Guidance, Control, and Dynamics Vol. 22, No. 4, 1999, pp. 507-512.
    • (1999) Journal of Guidance, Control, and Dynamics , vol.22 , Issue.4 , pp. 507-512
    • Barker, J.M.1    Balas, G.J.2    Blue, P.A.3
  • 3
    • 0034819199 scopus 로고    scopus 로고
    • Robust multivariable flutter suppression for benchmark active control technology wind-tunnel model
    • Waszak, M. R., "Robust Multivariable Flutter Suppression for Benchmark Active Control Technology Wind-Tunnel Model", Journal of Guidance, Control, and Dynamics Vol. 24, No. 1, 2001, pp. 147-153.
    • (2001) Journal of Guidance, Control, and Dynamics , vol.24 , Issue.1 , pp. 147-153
    • Waszak, M.R.1
  • 4
    • 0030151296 scopus 로고    scopus 로고
    • Robust control design strategy with parameter dominated uncertainty
    • May-June
    • Idan, M. and Shaviv, G.E., "Robust Control Design Strategy with Parameter Dominated Uncertainty", AIAA Journal of Guidance, Control and Duamics , Vol. 19, No. 3, May-June 1996, pp. 605-611.
    • (1996) AIAA Journal of Guidance, Control and Duamics , vol.19 , Issue.3 , pp. 605-611
    • Idan, M.1    Shaviv, G.E.2
  • 6
    • 0025207009 scopus 로고
    • Time-domain aeroservoelastic modeling using weighted unsteady aerodynamic forces
    • Karpel, M., "Time-Domain Aeroservoelastic Modeling Using Weighted Unsteady Aerodynamic Forces", Journal of Guidance, Control, and Dynamics, Vol.13, No. 1, 1990, pp. 30-37.
    • (1990) Journal of Guidance, Control, and Dynamics , vol.13 , Issue.1 , pp. 30-37
    • Karpel, M.1
  • 7
    • 0032629010 scopus 로고    scopus 로고
    • Aeroservoelastic interaction between aircraft structural and control design schemes
    • Idan, M., Karpel, M. and Moulin, B., "Aeroservoelastic Interaction between Aircraft Structural and Control Design Schemes", Journal of Guidance, Control, and Dynamics Vol. 22, No. 4, 1999, pp. 513-519.
    • (1999) Journal of Guidance, Control, and Dynamics , vol.22 , Issue.4 , pp. 513-519
    • Idan, M.1    Karpel, M.2    Moulin, B.3
  • 8
    • 0032715079 scopus 로고    scopus 로고
    • Reduced-order models for integrated aeroservoelastic optimization
    • Karpel, M., "Reduced-Order Models for Integrated Aeroservoelastic Optimization", Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 146-155.
    • (1999) Journal of Aircraft , vol.36 , Issue.1 , pp. 146-155
    • Karpel, M.1
  • 9
    • 0036178635 scopus 로고    scopus 로고
    • Match-point solutions for robust flutter analysis
    • Lind, R., "Match-Point Solutions for Robust Flutter Analysis", Journal of Aircraft, Vol. 39, No. 1, 2002, pp. 91-99.
    • (2002) Journal of Aircraft , vol.39 , Issue.1 , pp. 91-99
    • Lind, R.1
  • 11
    • 16244364434 scopus 로고    scopus 로고
    • Application of the state-space equation of the integrated system in stability and response analyses including sensitivity evaluation
    • TAE No. 899, Faculty of Aerospace Engineering, Technion - I.I.T., Haifa, Israel, July
    • Moulin, B., Feldgun, V. and Karpel, M., "Application of the State-Space Equation of the Integrated System in Stability and Response Analyses Including Sensitivity Evaluation", Technical Report, TAE No. 899, Faculty of Aerospace Engineering, Technion - I.I.T., Haifa, Israel, July 2002.
    • (2002) Technical Report
    • Moulin, B.1    Feldgun, V.2    Karpel, M.3
  • 13
    • 2342541614 scopus 로고    scopus 로고
    • ZONA Technology Inc., Scottsdale, AZ, November
    • ZAERO Version 7.0. Theoretical Manual, ZONA Technology Inc., Scottsdale, AZ, November 2003.
    • (2003) ZAERO Version 7.0. Theoretical Manual
  • 15
    • 85085773008 scopus 로고    scopus 로고
    • Extension of the g-method flutter solution to aeroservoelastic stability analysis
    • Proceedings of the 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Norfolk, Virginia, U.S.A., April 2003, AIAA Paper 2003-1512. In press
    • Karpel, M., Moulin, B. and Chen, P.C. "Extension of the g-Method Flutter Solution to Aeroservoelastic Stability Analysis", Proceedings of the 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Norfolk, Virginia, U.S.A., April 2003, AIAA Paper 2003-1512. In press in the AIAA Journal of Aircraft.
    • AIAA Journal of Aircraft
    • Karpel, M.1    Moulin, B.2    Chen, P.C.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.