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Volumn 22, Issue 2, 1999, Pages 278-285

Comparison of μ- and H2-Synthesis Controllers on an Experimental Typical Section

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; CONTROL SYSTEM SYNTHESIS; FEEDBACK CONTROL; FLUTTER (AERODYNAMICS); IDENTIFICATION (CONTROL SYSTEMS); SENSORS; SYSTEM STABILITY; WIND TUNNELS;

EID: 0033097449     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4375     Document Type: Article
Times cited : (25)

References (26)
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  • 3
    • 0029230530 scopus 로고
    • Design and Multifunction Tests of a Frequency Domain-Based Active Flutter Suppression System
    • Adams, W. M. J., and Christhilf, D. M., "Design and Multifunction Tests of a Frequency Domain-Based Active Flutter Suppression System," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 52-60.
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    • Adams, W.M.J.1    Christhilf, D.M.2
  • 4
    • 0029208273 scopus 로고
    • Flutter Suppression Control Law Design and Testing for the Active Flexible Wing
    • Mukhopadhyay, V., "Flutter Suppression Control Law Design and Testing for the Active Flexible Wing," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 45-51.
    • (1995) Journal of Aircraft , vol.32 , Issue.1 , pp. 45-51
    • Mukhopadhyay, V.1
  • 10
    • 84983165302 scopus 로고    scopus 로고
    • Modeling the Benchmark Active Control Technology Wind-Tunnel Model for Application to Flutter Suppression
    • (San Diego, CA), AIAA, Reston, VA
    • Waszak, M. R., "Modeling the Benchmark Active Control Technology Wind-Tunnel Model for Application to Flutter Suppression," Proceedings of the AIAA Atmospheric Flight Mechanics Conference (San Diego, CA), AIAA, Reston, VA, 1996.
    • (1996) Proceedings of the AIAA Atmospheric Flight Mechanics Conference
    • Waszak, M.R.1
  • 13
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    • IEEE Control Systems , vol.17 , Issue.4 , pp. 64-70
    • Haley, P.1    Soloway, D.2
  • 15
    • 0029179176 scopus 로고
    • Robustness Analysis of Controllers Designed for Active Flutter Suppression
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    • (1995) Proceedings of the American Control Conference , vol.1 , pp. 182
    • Tokur, O.1    Ozbay, H.2
  • 16
    • 0028464590 scopus 로고
    • ∞Controller Design for a Two-Dimensional Thin Airfoil Flutter Suppression
    • ∞Controller Design for a Two-Dimensional Thin Airfoil Flutter Suppression," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 4, 1994, pp. 722-728.
    • (1994) Journal of Guidance, Control, and Dynamics , vol.17 , Issue.4 , pp. 722-728
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  • 17
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    • Experimental Active Control of a Typical Section Using a Trailing Edge Flap
    • Vipperman, J. S., Clark, R. L., Conner, M. D., and Dowell, E. H., "Experimental Active Control of a Typical Section Using a Trailing Edge Flap," Journal of Aircraft, Vol. 35, No. 2, 1998, pp. 224-229.
    • (1998) Journal of Aircraft , vol.35 , Issue.2 , pp. 224-229
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  • 18
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    • Multivariable Active Lifting Surface Control Using Strain Actuation: Analytical and Experimental Results
    • San Diego, CA
    • Lazarus, K. B., and Crawley, E. F., "Multivariable Active Lifting Surface Control Using Strain Actuation: Analytical and Experimental Results," 3rd International Conf. on Adaptive Structures, San Diego, CA, Vol. 2040, 1993, pp. 87-101.
    • (1993) 3rd International Conf. on Adaptive Structures , vol.2040 , pp. 87-101
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.