Piezoelectric actuator optimization for simultaneous aircraft cabin noise and vibration control
Mots-clés :
Control system analysis, Genetic algorithms, Optimization, Piezoelectric devices, Propellers, Vibrations (mechanical), Aircraft cabin noise, Piezoelectric actuatorRésumé
The use of the piezoelectric (PZT) actuator optimization for simultaneous aircraft cabin noise and vibration control is effective in reducing both noise and vibration. The study explores PZT elements into different control groups as means to simplify the control systems while increasing the control authority. A genetic algorithm is developed to optimize the noise and vibration separately and independently. By the application of Pareto cooperative optimization approach the present work can be extended to both noise and vibration reduction performance.
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