Experimental Study on Piezoelectric-Stack-Actuator-Driven Active Vibration Control of Helicopter Floor Structure

No AccessEngineering NotesExperimental Study on Piezoelectric-Stack-Actuator-Driven Active Vibration Control of Helicopter Floor StructureDe Meng, Pinqi Xia, Laishou Song and Edward C. SmithDe MengNanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China*Ph.D. Candidate, College of Aerospace Engineering; .Search for more papers by this author, Pinqi XiaNanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China†Professor, College of Aerospace Engineering; (Corresponding Author).Search for more papers by this author, Laishou SongNanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China‡Associate Professor, College of Aerospace Engineering; .Search for more papers by this author and Edward C. SmithPennsylvania State University, University Park, Pennsylvania 16802§Professor, Department of Aerospace Engineering; .Search for more papers by this authorPublished Online:20 Dec 2019https://doi.org/10.2514/1.C035607SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Pearson J. T., Goodall R. M. and Lyndon I., “Active Control of Helicopter Vibration,” Computing & Control Engineering Journal, Vol. 5, No. 6, Dec. 1994, pp. 277–284. https://doi.org/10.1049/cce:19940608 CrossrefGoogle Scholar[2] Friedmann P. P. and Millott T. A., “Vibration Reduction in Rotorcraft Using Active Control: A Comparison of Various Approaches,” Journal of Guidance, Control, and Dynamics, Vol. 18, No. 4, Aug. 1995, pp. 664–673. https://doi.org/10.2514/3.21445 LinkGoogle Scholar[3] Hugin C. T., Hatch C., Skingle G. W. and Griffiths T. 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Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3868 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsActuatorsAeronauticsAvionicsBeam (Structures)Computational Fluid DynamicsFinite Element MethodFlexible and Active StructuresFluid DynamicsGuidance, Navigation, and Control SystemsMechanical and Structural VibrationsStress-Strain AnalysisStructural AnalysisStructural EngineeringStructures, Design and TestVibration ControlVibration Measuring Instruments KeywordsHelicoptersActive Vibration ControlPiezoelectric Stack ActuatorAirframesBlade Passing FrequencyFinite Element ModelingAdaptive Control AlgorithmAerospace EngineeringHarmonic ExcitationPilotAcknowledgmentsThis study has been supported by the National Natural Science Foundation of China (Grant No. 11572150) and by the funding of Jiangsu Innovation Program for Graduate Education (Grant No. KYLX15_0229, 2015).PDF Received24 May 2019Accepted24 October 2019Published online20 December 2019