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Vibration suppression and slewing control of a flexible structureExamined here are the effects of motor dynamics and secondary piezoceramic actuators on vibration suppression during the slewing of flexible structures. The approach focuses on the interaction between the structure, the actuators, and the choice of control law. The results presented here are all simulated, but are based on experimentally determined parameters for the motor, structure, piezoceramic actuators, and piezofilm sensors. The simulation results clearly illustrate that the choice of motor inertia relative to beam inertia makes a critical difference in the performance of the system. In addition, the use of secondary piezoelectric actuators reduces the load requirements on the motor and also reduces the overshoot of the tip deflection. The structures considered here are a beam and a frame. The majority of results are based on a Euler Bernoulli beam model. The slewing frame introduces substantial torsional modes and a more realistic model. The slewing frame results are incomplete and represent work in progress.
Document ID
19910013026
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Inman, Daniel J.
(Buffalo Univ. NY, United States)
Garcia, Ephrahim
(Buffalo Univ. NY, United States)
Pokines, Brett
(Buffalo Univ. NY, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Publication Information
Publication: NASA. Langley Research Center, Fourth NASA Workshop on Computational Control of Flexible Aerospace Systems, Part 2
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N22339
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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