Experimental Study on Piezoelectric-Stack-Actuator-Driven Active Vibration Control of Helicopter Floor Structure
JOURNAL OF AIRCRAFT(2020)
摘要
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. J., “Active Vibration Control of the Lynx Helicopter Airframe,” 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference Proceedings, AIAA Paper 2007-2222, April 2007. https://doi.org/10.2514/6.2007-2222 LinkGoogle Scholar[4] Lee T. and Chopra I., “Design of Piezostack-Driven Trailing-Edge Flap Actuator for Helicopter Rotors,” Smart Materials & Structures, Vol. 10, No. 1, 2001, pp. 15–24. https://doi.org/10.1088/0964-1726/10/1/302 CrossrefGoogle Scholar[5] Simões R. C., Steffen V., Hagopian J. D. and Mahfoud J., “Modal Active Vibration Control of a Rotor Using Piezoelectric Stack Actuators,” Journal of Vibration and Control, Vol. 13, No. 1, 2007, pp. 45–64. https://doi.org/10.1177/1077546306070227 CrossrefGoogle Scholar[6] Singhvi R. and Vennkatesan C., “Vibration Control of an Idealized Helicopter Model Using Piezo Stack Sensor-Actuator,” 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural, Dynamics, and Materials Conference Proceedings, AIAA Paper 2005-2275, April 2005. https://doi.org/10.2514/6.2005-2275 LinkGoogle Scholar[7] Hanagud S. and Babu G. L., “Smart Structures in the Control of Airframe Vibrations,” Journal of American Helicopter Society, Vol. 39, No. 2, 1994, pp. 69–72. https://doi.org/10.4050/JAHS.39.69 CrossrefGoogle Scholar[8] Heverly D., Wang K. W. and Smith E. C., “An Optimal Actuator Placement Methodology for Active Control of Helicopter Airframe Vibrations,” Journal of American Helicopter Society, Vol. 46, No. 4, 2001, pp. 251–261. https://doi.org/10.4050/JAHS.46.251 CrossrefGoogle Scholar[9] Walchko J. C., Wang K. W., William E., Kim J. S. and Smith E. C., “Hybrid Feedforward-Feedback Control for Active Helicopter Vibration Suppression,” Proceeding of the 63rd Annual Forum of the American Helicopter Society, AHS International, Fairfax, VA, May 2007, pp. 1757–1773. Google Scholar[10] Song L. and Xia P., “Active Control of Helicopter Structural Response Using Piezoelectric Stack Actuators,” Journal of Aircraft, Vol. 50, No. 2, March 2013, pp. 659–663. https://doi.org/10.2514/1.C031758 LinkGoogle Scholar[11] Song L. and Xia P., “A Harmonic Synchronous Identification Updating Method for Active Control of Helicopter Structural Response Driven by Piezoelectric Stack Actuators,” Journal of the American Helicopter Society, Vol. 60, No. 3, 2015, Paper 032013. https://doi.org/10.4050/JAHS.60.032013 CrossrefGoogle Scholar[12] Meng D., Xia P. and Song L., “MIMOMH Feed-Forward Adaptive Vibration Control of Helicopter Fuselage by Using Piezoelectric Stack Actuators,” Journal of Vibration and Control, Vol. 24, No. 23, Dec. 2018, pp. 5534–5545. https://doi.org/10.1177/1077546318757840 CrossrefGoogle Scholar[13] Mizuno M., Enomoto Y. and Okayasu M., “Fatigue Life of Piezoelectric Ceramics and Evaluation of Internal Damage,” Procedia Engineering, Vol. 2, No. 1, 2010, pp. 291–297. https://doi.org/10.1016/j.proeng.2010.03.032 CrossrefGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byProgress of Study on the Application of Actuators in Helicopter Airframe ACSRs1 January 2023New Algorithm and Experiments for Helicopter Active Control of Structural ResponseKai Lang, Pinqi Xia and Lina Shang14 February 2022 | Journal of Aircraft, Vol. 59, No. 5Smart Active Vibration Control System of a Rotary Structure Using Piezoelectric Materials29 July 2022 | Sensors, Vol. 22, No. 15Research and Implementation of Vector Control Strategy for Centrifugal ActuatorResearch and Implementation of SVPWM Control Strategy for Centrifugal ActuatorHybrid feedback PID-FxLMS algorithm for active vibration control of cantilever beam with piezoelectric stack actuatorJournal of Sound and Vibration, Vol. 509 What's Popular Volume 57, Number 2March 2020 CrossmarkInformationCopyright © 2019 by the authors. 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
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