Piezoelectric Actuators as Control Surfaces for Morphing Vehicle

Author:

Mennu M. M.,Tran B.,Ifju P. G.

Publisher

Springer International Publishing

Reference7 articles.

1. Barbarino, S., Bilgen, O., Ajaj, R.M., Friswell, M.I., Inman, D.J.: A review of morphing aircraft. J. Intell. Mater. Syst. Struct. 22(9), 823–877 (2011)

2. Ohanian, O., et al.: Piezoelectric morphing versus servo-actuated MAV control surfaces. In: 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
20th AIAA/ASME/AHS Adaptive Structures Conference
14th AIAA (2012)

3. Bilgen, O., Kochersberger, K., Diggs, E.C., Kurdila, A.J., Inman, D.J.: Morphing wing micro-air-vehicles via macro-fiber-composite actuators. In: Collection of Technical Papers—AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol. 1, pp. 1005–1020 (2007)

4. Lacroix, B.W., Ifju, P.G.: Aeroelastic model for macrofiber composite actuators on micro air vehicles. J. Aircr. 54(1), 199–208 (2017)

5. J. W. High and W. K. Wilkie, “Method of Fabricating NASA-Standard Macro-Fiber Composite Piezoelectric Actuators,” 2003.

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