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Aiaa 2008 6490

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AIAA-2008-6490 Transition Point Displacement Control on a Wing Equipped with Actuators A. Popov, M. Labib, J. Fays and R. Botez, ETS, Montreal, Quebec, Canada
SUMMARY ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Project context ,[object Object],[object Object],[object Object],[object Object],[object Object]
Project context Morphing wing schematic concept
Project context ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Simplified model ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Simplified model
SMA model in open loop Shape memory and super-elasticity properties of Ni-Ti alloys Shape memory actuators principle
SMA model in open loop ,[object Object],Delay due to phase transformation :
SMA model in open loop
SMA model control in closed loop ,[object Object],[object Object]
SMA model control in closed loop ,[object Object],K P = 144.28, K I = 11.10 K D = 332.96
SMA model control in close loop ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
SMA model control in close loop
Aerodynamic simulation of the simplified model controlled by SMA in close loop ,[object Object],[object Object],[object Object]
Aerodynamic simulation of the simplified model controlled by SMA in close loop Simulation results
Bench test Charging spring Linear variable differential transducer Force transducer Wheel Potentiometer error < ± 0,005 mm Heating generated by PID Cooling current = 0
Conclusion ,[object Object],[object Object],[object Object]
Future work ,[object Object]
Future work ,[object Object],[object Object],[object Object]

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Aiaa 2008 6490