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• W2322754581 abstract "The use of piezo-ceramic actuators for UAV ight control has been shown to be e ective both in the wind tunnel and in ight test. Macro ber composite (MFC) actuators are a high strain variant of the lead zirconate titanate (PZT) actuator, and have been employed in a bimorph con guration to cause morphing camber control of aerodynamic surfaces in less than 0.5 m wingspan UAV applications. One of the challenges of operating these conformal actuators is to quantify the voltage input/displacement output relationship given hysteresis and aerodynamic loading e ects. The work presented provides a framework for the practical implementation of these actuators by using both open and closed loop feedback systems for displacement control. Results are presented for thick airfoil designs where only the trailing edge is de ected using smart materials. The two main sources of non-linear behavior include dynamic pressure and actuator hysteresis, and knowledge of these parameters can be used for reasonably good open loop displacement control. Results are presented for 2-D airfoil section testing." @default.
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• W2322754581 date "2012-01-09" @default.
• W2322754581 modified "2023-09-27" @default.
• W2322754581 title "Smart material actuators as a means of UAV flight control" @default.
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• W2322754581 doi "https://doi.org/10.2514/6.2012-486" @default.
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