New adaptive controller method for SMA hysteresis modelling of a morphing wing
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[1] Bart Kosko,et al. Neural networks and fuzzy systems: a dynamical systems approach to machine intelligence , 1991 .
[2] S. Sivanandam,et al. Introduction to Fuzzy Logic using MATLAB , 2006 .
[3] Armando R. Rodriguez. Morphing Aircraft Technology Survey , 2007 .
[4] Chung-Chun Kung,et al. Affine Takagi-Sugeno fuzzy modelling algorithm by fuzzy c-regression models clustering with a novel cluster validity criterion , 2007 .
[5] Ruxandra Botez,et al. Transition Point Detection from the Surface Pressure Distribution for Controller Design , 2008 .
[6] Mahdi Mahfouf,et al. Fuzzy Takagi-Sugeno Kang model predictive control for process engineering , 1999 .
[7] G. Song,et al. A Neural Network Inverse Model for a Shape Memory Alloy Wire Actuator , 2003 .
[8] David J. Moorhouse,et al. Benefits and design challenges of adaptive structures for morphing aircraft , 2006, The Aeronautical Journal (1968).