Paper
14 October 2003 System design for active vibration control of aerospace structures
V. Shankar, B. V. Nagaraja, R. Balasubramaniam, Amrutha Shree S, Skanda N. Muthaiah
Author Affiliations +
Proceedings Volume 5062, Smart Materials, Structures, and Systems; (2003) https://doi.org/10.1117/12.514634
Event: Smart Materials, Structures, and Systems, 2002, Bangalore, India
Abstract
Instrumentation, electronics, digital signal processing and related software form the basic building blocks of a system for implementation of Active Vibration Control (AVC) for smart aerospace structures. This paper essentially deals with the design, development and implementation of a 4 channel analog input sub-system essentially consisting of charge amplifiers, filters, gain amplifiers & Analog to Digital Converters (ADC), the subsequent Digital Signal Processor (DSP) hardware for implementation of the controller and finally a 4 Channel analog output subsystem consisting of Digital to Analog Converters (DAC), reconstruction filters & high voltage amplifiers. This system essentially interfaces to a structure with piezo-ceramic sensors and actuators for implementation of real time AVC on a smart beam. The paper also highlights some of the new ideas that have been incorporated into the system design.
© (2003) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
V. Shankar, B. V. Nagaraja, R. Balasubramaniam, Amrutha Shree S, and Skanda N. Muthaiah "System design for active vibration control of aerospace structures", Proc. SPIE 5062, Smart Materials, Structures, and Systems, (14 October 2003); https://doi.org/10.1117/12.514634
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KEYWORDS
Digital signal processing

Amplifiers

Signal processing

Data acquisition

Sensors

Signal generators

Actuators

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