Paper
26 April 1996 Piezoceramics/CFRP composites for active vibration control and shape control of aerospace structures
Ursula Herold-Schmidt, Wolfgang Schaefer, Helmut W. Zaglauer
Author Affiliations +
Abstract
The application of piezoceramics/CFRP composites for active control of aerospace structures was investigated in a laboratory scale. Exemplary results are presented for active vibration damping of CFRP plates with integrated PZT sensors and actuators as well as for shape control of an antenna reflector shell using piezoelements.
© (1996) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Ursula Herold-Schmidt, Wolfgang Schaefer, and Helmut W. Zaglauer "Piezoceramics/CFRP composites for active vibration control and shape control of aerospace structures", Proc. SPIE 2779, 3rd International Conference on Intelligent Materials and 3rd European Conference on Smart Structures and Materials, (26 April 1996); https://doi.org/10.1117/12.237042
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Cited by 5 scholarly publications.
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KEYWORDS
Composites

Active vibration control

Aerospace engineering

Actuators

Antennas

Reflectors

Ferroelectric materials

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