Control on a 2-D Wing Flutter Using an Adaptive Nonlinear Neural Controller
An adaptive nonlinear neural controller to reduce the nonlinear flutter in 2-D wing is proposed in the paper. The nonlinearities in the system come from the quasi steady aerodynamic model and torsional spring in pitch direction. Time domain simulations are used to examine the dynamic aero elastic i...
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| Auteurs principaux: | , , |
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| Format: | article |
| Langue: | EN |
| Publié: |
Al-Khwarizmi College of Engineering – University of Baghdad
2018
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| Sujets: | |
| Accès en ligne: | https://doaj.org/article/dee9ba0949da4759963e23dd2e886bfb |
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