A hybrid fuzzy logic proportional integral derivative plus conventional on-off controller for a morphing wing actuation using shape memory alloys

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  1. National Research Council of Canada. Aerospace
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Conference52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, April 4-7, 2011, Denver, Colorado, USA
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Peer reviewedYes
NPARC number23001790
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