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Energy harvesting / Piezoelectricity / Transducers / Slew / Active vibration control / Attitude control / Spacecraft / Vibration / Modulation / Spaceflight / Physics / Electrical phenomena


www.elsevier.com/locate/actaastro PII: S0094[removed]Acta Astronautica Vol. 49, No. 2, pp. 73–83, 2001 ? 2001 Elsevier Science Ltd. All rights reserved
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Document Date: 2009-05-29 16:12:26

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Monterey / Akron / /

Company

Elsevier Science Ltd. / /

Country

United States / United Kingdom / /

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Facility

The University of Akron / /

IndustryTerm

energy levels / smart structure technology / energy level / Real time code / structural control applications / sub-systems / mode energy level / Cold gas jet thrusters / oE devices / control processor / attitude control sub-systems / space applications / real time control processor / downloaded control law / real-time control system / /

Organization

VIBRATION SUPPRESSION OF FLEXIBLE SPACECRAFT DURING ATTITUDE CONTROL GANGBING SONG† Department of Mechanical Engineering / US Federal Reserve / BRIJ N. AGRAWAL Aeronautics and Astronautics Department / University of Akron / Naval Postgraduate School / /

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Position

†Corresponding author / PD controller / bangbang controller / PPF controller / controller / /

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Harman On Time Radio / /

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Simulink / /

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Ohio / California / /

Technology

smart structure technology / TI-C30 real time control processor / real-time operating system / control processor / DSP / /

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www.elsevier.com/locate/actaastro / /

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