Modal Identification of Truss Structures by Changing Stiffness Using Piezoelectric Actuator
Author:
Affiliation:
1. Nagoya University, Nagoya, Aichi 464-8603, Japan
2. Tokyo Institute of Technology, Yokohama, Kanagawa 226-8502, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.35272
Reference37 articles.
1. Identification of vibrating flexible structures
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1. On-orbit modal identification for vibration suppression of flexible aerospace structure using reaction wheel actuator;Aerospace Science and Technology;2020-12
2. Active vibration control of a hoop truss structure with piezoelectric bending actuators based on a fuzzy logic algorithm;Smart Materials and Structures;2018-07-25
3. Methods for the vibration determination and parameter identification of spacecraft with flexible structures;Journal of Computer and Systems Sciences International;2017-03
4. Recursive Self-identification and Its Transient Response Analysis with Extended Kalman Filter;Journal of Aerospace Computing, Information, and Communication;2012-10
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