Vibration Control of an Idealized Helicopter Model Using Piezo Stack Sensor- Actuator

机译：使用压电堆栈传感器-执行器的理想直升机模型的振动控制

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《AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference;AIAA/ASME/AHS Adaptive Structures Conference;AIAA Non-Deterministic Approaches Forum;AIAA Gossamer Spacecraft Forum;AIAA Multidisciplinary Design Optimization Specialist Conference》|2005年|P.1-19|共19页
会议地点 Austin, TX(US);Austin, TX(US);Austin, TX(US);Austin, TX(US);Austin, TX(US)
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R. Singhvi; C. Venkatesan;
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Indian Institute of Technology Kanpur Kanpur India;

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入库时间 2022-08-26 14:42:21

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2. Mu-Synthesis robust control of 3D bar structure vibration using piezo-stack actuators [J] . Arkadiusz Mystkowski, Andrzej Piotr Koszewnik Mechanical systems and signal processing . 2016,第octa期

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3. Feasibility study on a hybrid mount system with air springs and piezo-stack actuators for microvibration control [J] . Dong-Doo Jang, Hyung-Jo Jung, Yun-Ho Shin, Journal of intelligent material systems and structures . 2012,第5期

机译：带有空气弹簧和压电堆栈执行器的微振动控制混合安装系统的可行性研究
4. Vibration Control of an Idealized Helicopter Model Using Piezo Stack Sensor- Actuator [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/American Society of Civil Engineers/American Helicopter Society/ASC Structures, Structural Dynamics Materials Conference . 2005

机译：使用压电堆传感器 - 致动器的理想直升机模型的振动控制
5. Optimal actuator placement and active structure design for control of helicopter airframe vibrations. [D] . Heverly, David Ellsworth, II. 2002

机译：最佳的执行器位置和主动结构设计可控制直升机机身的振动。
6. A Compound Control Based on the Piezo-Actuated Stage with Bouc–Wen Model [O] . Jiwen Fang, Jia Wang, Chong Li, 2019

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7. Hysteresis Characterization in Piezoceramic Stack Actuators and Its Influence on Vibration and Noise Reduction in Helicopters Using Actively Controlled Flaps [O] . Eric Muir, Li Liu, Peretz Friedmann, 2010

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Vibration Control of an Idealized Helicopter Model Using Piezo Stack Sensor- Actuator

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