Vibration Control Of Flexible Spacecraft Integrating A Momentum Exchange Controller And A Distributed Piezoelectric Actuator

DOI10.1006/jsvi.1994.1450zbMath0945.74650OpenAlexW2042587929MaRDI QIDQ4493807

Publication date: 22 August 2000

Published in: Journal of Sound and Vibration (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1006/jsvi.1994.1450

Mathematics Subject Classification ID

Control, switches and devices (``smart materials) in solid mechanics (74M05) Vibrations in dynamical problems in solid mechanics (74H45) Thin bodies, structures (74K99)

Related Items (4)

Semi-analytical solutions of static and dynamic degenerate, nondegenerate and functionally graded electro-elastic multilayered plates ⋮ Stabilisation of a flexible spacecraft subject to external disturbance and uncertainties ⋮ Dynamics and control of a smart flexible satellite moving in an orbit ⋮ Discussion on: ``Adaptive variable structure maneuvering control and vibration reduction of three-axis stabilized flexible spacecraft

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