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T.L. Grigorie, A.V. Popov,  R.M. Botez, Y. Mébarki, and M. Mamou (Canada) The International Association of Science and Technology for Development (IASTED) Identification, Control and Applications Conference ~ICA 2009~  Honolulu, Hawaii August 17 – 19, 2009
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],[object Object],[object Object]
Project context ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Experimental setup description ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],From the initial studies related to the  optimal configuration  of the flexible structure,  two actuation lines , positioned at 25.3% and 47.6% of the chord from the airfoil leading edge.
Model of the flexible structure The reference airfoil is the NLF airfoil, WTEA.
Experimental setup description ,[object Object],[object Object],[object Object],[object Object],C135 C128 C121 C114 C107 2 o 7 C134 C127 C120 C113 C106 1.5 o 6 C133 C126 C119 C112 C105 1 o 5 C132 C125 C118 C111 C104 0.5 o 4 C131 C124 C117 C110 C103 0 o 3 C130 C123 C116 C109 C102 -0.5 o 2 C129 C122 C115 C108 C101 -1 o 1 0.3 0.275 0.25 0.225 0.2 α [ o ] 5 4 3 2 1 Mach
Experimental setup description ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Open loop control ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Experimental results PID controller  Self tuning fuzzy controller  Ladder command  self tuning fuzzy controller
Experimental results ,[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Real time signal acquisition
[object Object],[object Object],[object Object],Data acquisition
Infrared visualization ,[object Object],M  = 0.3,    = -1°  M  = 0.275,    = 0° Morphing  Rigid Rows of pressure sensors Lines of SMA actuators 45% 66% a) b) 33% 57% a) b)
Conclusion ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

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Iasted Open Loop

  • 1. T.L. Grigorie, A.V. Popov, R.M. Botez, Y. Mébarki, and M. Mamou (Canada) The International Association of Science and Technology for Development (IASTED) Identification, Control and Applications Conference ~ICA 2009~ Honolulu, Hawaii August 17 – 19, 2009
  • 2.
  • 3.
  • 4.
  • 5.
  • 6. Model of the flexible structure The reference airfoil is the NLF airfoil, WTEA.
  • 7.
  • 8.
  • 9.
  • 10. Experimental results PID controller Self tuning fuzzy controller Ladder command self tuning fuzzy controller
  • 11.
  • 12.
  • 13.
  • 14.
  • 15.