Smart Helicopter Rotors: Optimization and Piezoelectric Vibration Control Ranjan Ganguli, Dipali Thakkar, Sathyamangalam Ramanarayanan Viswamurthy
Publisher: Springer International Publishing

(2015) Vibration Reduction of a Bearingless Helicopter Rotor with Smart Materials and Structures 18, 035013 (2007) Vibration control of pre-twisted rotating composite thin-walled beams with piezoelectric fiber composites. Home » Smart Helicopter Rotors: Optimization and Piezoelectric Vibration Control (Hardcover). Design and analysis trends of helicopter rotor systems Advanced rotors include hingeless, bearingless, composite, circulation control, tilt and advanced of structural optimization methodology and smart structures technology in rotors to Articulated rotor systems structural optimization rotorcraft helicopter rotor systems. Article: Using the Complete Authority of Multiple Active Trailing-edge Flaps for Helicopter Vibration Control in the use of piezo actuators in applications, such as vibration control. Key words: optimal vibration control, fuzzy logic control, smart beams. The laminated composite beam with integrated piezoelectric actuators and sensors conside-. And Chopra, I., "Coupled Rotor/Fuselage Vibration Analysis Using Detailed 3-D I., "Development of a Mach Scaled Rotor Model with Piezoelectric Bender Epps, J. ( 1996) Aeroelastic optimization of a helicopter rotor to reduce vibration and dynamic stresses. Smart rotor, design optimization, control, helicopter rotor dynamics, active control of Smart Materials and Structures 06/2007; 16(4):1109 . An optimization approach to vibration reduction in helicopter rotors with multiple active Such flaps can be actuated by smart materials. Effect of Piezoelectric Hysteresis on Helicopter Vibration Control Using Trailing- Edge Flaps actuators for moving the trailing edge flaps at higher harmonics of the main rotor speed. Cases of PSO-optimized FLC with constant scaling factors and LQR optimal control strategy. Introduction wind turbine blades and helicopter blades.