Development of a resonant trailing-edge flap actuation system for helicopter rotor vibration control
Authors:
- J-S KimJKJ-S Kim
- K W WangKWK W Wang
- E C SmithESE C Smith
- 10 October 2007
- journal article
- Published by IOP Publishing in Smart Materials and Structures
- Vol. 16 (6) , 2275-2285
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- High-authority Piezoelectric Actuation System Synthesis through Mechanical Resonance and Electrical TailoringJournal of Intelligent Material Systems and Structures, 2005
- Rotary-Wing Aeroelasticity: Current Status and Future TrendsAIAA Journal, 2004
- Optimization and implementation of multimode piezoelectric shunt damping systemsIEEE/ASME Transactions on Mechatronics, 2002
- Induced-shear piezoelectric actuators for rotor blade trailing edge flapsSmart Materials and Structures, 2002
- Active-passive hybrid piezoelectric networks for vibration control: comparisons and improvementSmart Materials and Structures, 2001
- Hover Testing of a Small-Scale Rotor with On-Blade ElevonsJournal of the American Helicopter Society, 2001
- Design of piezostack-driven trailing-edge flap actuator for helicopter rotorsSmart Materials and Structures, 2001
- Phase control approach to hysteresis reductionIEEE Transactions on Control Systems Technology, 2001
- Analysis and Testing of Mach-Scaled Rotor with Trailing-Edge FlapsAIAA Journal, 2000
- Damping of structural vibrations with piezoelectric materials and passive electrical networksJournal of Sound and Vibration, 1991