Optics and Precision Engineering, Volume. 22, Issue 6, 1538(2014)
Integrated design optimization of actuator structural parameters and control voltages for morphing structural shapes
[2] [2] SOLFA A Y N, MEGUID S A, TAN K T, et al.. Shape morphing of aircraft wing: status and challenges [J]. Materials and Design, 2010, 31: 1284-1292.
[4] [4] SILVESTRO B, ONUR B, RAFIC M A, et al.. A review of morphing aircraft [J]. Journal of Intelligent Material Systems and Structures, 2011, 22: 823-877.
[5] [5] BARBARINO S, AMEDURI S, LECCE L. Wing shape control through an SMA-based device[J]. Journal of Intelligent Material Systems and Structures, 2009, 20:283-296.
[6] [6] KAPURIA S, YASIN M Y. Active vibration control of piezoelectric laminated beams with electroded actuators and sensors using an efficient finite element involving an electric node [C]. Smart Mater. Struct. IOP Publishing Ltd,USA, 2010: 045019(1-15).
[7] [7] WEI Q, ZHANG CH J, ZHANG D,et al.. Neural network control for piezo-actuator using sliding-mode technique [J]. Opt. Precision Eng., 2012, 20(5):1055-1063.
[8] [8] GU Y, TONG L Y, TAN P. Surface strain distribution method for delamination detection using piezoelectric actuators and sensors[C]. Journal of Physics: Conference Series., DAMAS, 2011: 012077(1-10).
[9] [9] LIU S T, LIN ZH Q. Design optimization of actuator-controller linkage scheme for morphing structural shapes [J]. Engineering Mechanics, 2009, 2(26):227-233. (in Chinese)
[10] [10] NIE R, QIU J H, JI H L. A design of honeycomb sandwich based on piezoelectric fiber composites[C]. Proceedings of the 2010 Symposium on Piezoelectricity, Acoustic Waves and Device Applications, 2010: 366-370. (in Chinese)
[11] [11] BENT A A. Active fiber composites for structural actuation [D]. Massachusetts: Massachusetts Institute of Technology, 1997.
[12] [12] BOWEN C R, NELSON L J, STEVENS R, et al.. Optimisation of interdigitated electrodes for piezoelectric actuators and active fiber composites [J]. Journal of Electroceramics, 2006, 16: 263-269.
[13] [13] LIN X J, ZHANG D, ZHANG X Y, et al.. Modeling and optimization of piezoelectric fiber composites based on finite element method [J]. The Chinese Journal of Nonferrous Metals, 2012, 22(6): 1748-1753. (in Chinese)
[14] [14] LIU Y ZH, ZHANG Y C, LIU SH T. Layout optimization design of wing structures with consideration of stability of composite skin [J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(10): 1985-1992. (in Chinese)
[15] [15] VASISTA S, TONG L Y. Pressurized morphing wing structures [C]. 53rd AIAA/ ASME/ ASCE/ AHS/ ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2006: 2414(1-11).
[16] [16] VASISTA S, TONG L Y, WONG K C. Realization of morphing wings: A multidisciplinary challenge [J]. Journal of Aircraft, 2012, 49(1):11-28.
[17] [17] LUO Z, TONG L Y, LUO J Z, et al.. Design of piezoelectric actuators using a multiphase level set method of piecewise constants [J]. Journal of Computational Physics, 2009, 228: 2643-2659.
[18] [18] VASISTA S, TONG L Y. Design and testing of pressurized cellular planar morphing structures [J]. AIAA Journal, 2012, 50(6):1328- 1338.
[19] [19] LI M, CHEN W M, WANG M CH, et al..A load simulation method of piezoelectric actuator in FEM for smart structures [J]. Sci. China Ser. E-Tech. Sci, 2009, 52(9): 2576-2584. (in Chinese)
[20] [20] MARTINEZ M, ARTEMEV A. Finite element analysis of broken fiber effects on the performance of active fiber composites [J]. Composite Structures, 2009, 88(3): 491-496.
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GAO Ren-jing, ZHANG Ying, WU Shu-hao, LIU Shu-tian. Integrated design optimization of actuator structural parameters and control voltages for morphing structural shapes[J]. Optics and Precision Engineering, 2014, 22(6): 1538
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Received: Dec. 5, 2013
Accepted: --
Published Online: Jun. 30, 2014
The Author Email: Ren-jing GAO (renjing@dlut.edu.cn)