Active Control of Helicopter Structural Response Using Piezoelectric Stack Actuators

No AccessEngineering NoteActive Control of Helicopter Structural Response Using Piezoelectric Stack ActuatorsLaishou Song and Pinqi XiaLaishou SongLaboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China*Ph.D. Candidate, Laboratory of Rotorcraft Aeromechanics.Search for more papers by this author and Pinqi XiaLaboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China†Professor, Laboratory of Rotorcraft Aeromechanics; (Corresponding Author).Search for more papers by this authorPublished Online:30 Mar 2013https://doi.org/10.2514/1.C031758SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Joshi A., Shourie A., Mujumdar P. and Joshi A., “Active Vibration Control of Scaled Wing Box Model Using Piezoelectric Stack Actuators,” 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA Paper 2008-1728, April 2008. LinkGoogle Scholar[2] Walchko J. C., Kim J. S. and Wang K. W., “Hybrid Feedforward-Feedback Control for Active Helicopter Vibration Suppression,” Proceedings of the 63rd American Helicopter Society Annual Forum, AHS International, Alexandria, VA, May 2007. Google Scholar[3] Arbel A., “Controllability Measures and Actuator Placement in Oscillatory Systems,” International Journal of Control, Vol. 33, No. 3, 1981, pp. 565–574. doi:https://doi.org/10.1080/00207178108922941 IJCOAZ 0020-7179 CrossrefGoogle Scholar[4] Yang Y., Jin Z. and So C. K., “Integrated Optimal Design of Vibration Control System for Smart Beams Using Genetic Algorithms,” Journal of Sound and Vibration, Vol. 282, Nos. 3–5, 2005, pp. 1293–1307. doi:https://doi.org/10.1016/j.jsv.2004.03.048 JSVIAG 0022-460X CrossrefGoogle Scholar[5] Liu W., Hou Z. and Demetriou M. A., “A Computational Scheme for the Optimal Sensor/Actuator Placement of Flexible Structures Using Spatial H2 Measures,” Mechanical Systems and Signal Processing, Vol. 20, No. 4, 2006, pp. 881–895. doi:https://doi.org/10.1016/j.ymssp.2005.08.030 0888-3270 CrossrefGoogle Scholar[6] Roy T. and Chakraborty D., “Optimal Vibration Control of Smart Fiber Reinforced Composite Shell Structures Using Improved Genetic Algorithm,” Journal of Sound and Vibration, Vol. 319, Nos. 1–2, 2009, pp. 15–40. doi:https://doi.org/10.1016/j.jsv.2008.05.037 JSVIAG 0022-460X CrossrefGoogle Scholar[7] Hanagud S. and Babu G. L. N., “Smart Structures in the Control of Airframe Vibrations,” Journal of the American Helicopter Society, Vol. 39, No. 2, 1994, pp. 69–72. doi:https://doi.org/10.4050/JAHS.39.69 JHESAK 0002-8711 CrossrefGoogle Scholar[8] 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, AIAA Paper 2005-2275, April 2005. LinkGoogle Scholar[9] Heverly D., Wang K. W. and Smith E. C., “An Optimal Actuator Placement Methodology for Active Control of Helicopter Airframe Vibrations,” Journal of the American Helicopter Society, Vol. 46, No. 4, 2001, pp. 251–261. doi:https://doi.org/10.4050/JAHS.46.251 JHESAK 0002-8711 CrossrefGoogle Scholar[10] Rao S. S., Pan T.-S. and Venkayya V. B., “Optimal Placement of Actuator in Actively Controlled Structures Using Genetic Algorithms,” AIAA Journal, Vol. 29, No. 6, 1991, pp. 942–943. doi:https://doi.org/10.2514/3.10683 AIAJAH 0001-1452 LinkGoogle Scholar[11] Giurgiutiu V. and Rogers C. A., “Power and Energy Characteristics of Solid-State Induced-Strain Actuators for Static and Dynamic Application,” Journal of Intelligent Material Systems and Structures, Vol. 8, No. 9, 1997, pp. 738–750. doi:https://doi.org/10.1177/1045389X9700800903 JMSSER 1045-389X CrossrefGoogle Scholar[12] Deep K. and Singh K. P., “A Real Coded Genetic Algorithm for Solving Integer and Mixed Integer Optimization Problems,” Applied Mathematics and Computation, Vol. 212, No. 2, 2009, pp. 505–518. doi:https://doi.org/10.1016/j.amc.2009.02.044 AMHCBQ 0096-3003 CrossrefGoogle Scholar[13] Haykin S., Adaptive Tilter Theory, 4th ed., Prentice–Hall, Upper Saddle River, NJ, 2003, pp. 208–213. Google Scholar Previous article Next article