Dynamic Analysis of Flexible Truss with Clearance Joints and Vibration Control Based on Piezoelectric Active Strut-Reference-Cited by-同舟云学术

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Dynamic Analysis of Flexible Truss with Clearance Joints and Vibration Control Based on Piezoelectric Active Strut

Published:2022-10-11 Issue: Volume: Page:
ISSN:
Container-title:2022 16th Symposium on Piezoelectricity, Acoustic Waves, and Device Applications (SPAWDA)
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Author:

Wei Qiu-Qiu¹,Hu Kai-Ming¹,Xu Peng²,Li Hua³

Affiliation:

1. China Jiliang University,College of Mechanical and Electrical Engineering,Hangzhou,P. R. China,310018

2. Huzhou institute of Zhejiang University,Huzhou,P. R. China,313002

3. Zhejiang University,College of Aeronautics and Astronautics,Hangzhou,P. R. China,310007

Funder

China Postdoctoral Science Foundation

National Natural Science Foundation of China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10045834/10045835/10045901.pdf?arnumber=10045901

Reference10 articles.

1. Dynamics and control of rigid-flexible coupling flexible spacecraft with joint clearance;sun;Chinese Journal of Theoretical and Applied Mechanics,2020

2. Active vibration control of a space truss using a lead zirconate titanate satack actuator;song;Proc Inst Mech Eng B J Eng Manuf,2001

3. Placement optimization of actuator and sensor and decentralized adaptive fuzzy vibration control for large space intelligent truss structure

4. Dynamic analysis of planar rigid-flexible coupling deployable solar array system with multiple revolute clearance joints;yy;Mech Syst Signal Process,2019

5. Dynamic simulation of deployment and locking of spacecraft solar panel using ADAMS;bai;Machinery Design & Manufacture,2006

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