Paper
8 September 1993 ACESA active-member damping performance
Allen J. Bronowicki, John W. Innis, Robert S. Betros, Steven P. Kuritz, Steven Fulton Griffin
Author Affiliations +
Abstract
The performance of the Advanced Composites with Embedded Sensors and Actuators (ACESA) vibration control system is described. The system consists of: three tubular active members sixteen feet long and five inches in diameter, with embedded piezoceramics (PZTs) allowing control of deformation axially and in two bending planes; a 9-channel digitally programmable analog local vibration control electronics unit; and 400 Volt drive electronics for each strut. The system is installed on a space based laser structural simulator at the AF Phillips Lab's Advanced Space Structure Research Experiments (ASTREX) facility at Edwards Air Force Base. The system has demonstrated ability to settle vibrations after a thruster induced slew in 0.2 seconds.
© (1993) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Allen J. Bronowicki, John W. Innis, Robert S. Betros, Steven P. Kuritz, and Steven Fulton Griffin "ACESA active-member damping performance", Proc. SPIE 1917, Smart Structures and Materials 1993: Smart Structures and Intelligent Systems, (8 September 1993); https://doi.org/10.1117/12.152813
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Cited by 5 scholarly publications.
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KEYWORDS
Actuators

Sensors

Ferroelectric materials

Control systems

Intelligence systems

Analog electronics

Smart structures

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