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Modified independent modal space control method for active control of flexible systemsA modified independent modal space control (MIMSC) method is developed for designing active vibration control systems for large flexible structures. The method accounts for the interaction between the controlled and residual modes. It incorporates also optimal placement procedures for selecting the optimal locations of the actuators in the structure in order to minimize the structural vibrations as well as the actuation energy. The MIMSC method relies on an important feature which is based on time sharing of a small number of actuators, in the modal space, to control effectively a large number of modes. Numerical examples are presented to illustrate the application of the method to generic flexible systems. The results obtained suggest the potential of the devised method in designing efficient active control systems for large flexible structures.
Document ID
19870014547
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Baz, A.
(Catholic Univ. of America, Washington, DC, United States)
Poh, S.
(Catholic Univ. of America, Washington, DC, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1987
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-181065
NAS 1.26:181065
Report Number: NASA-CR-181065
Report Number: NAS 1.26:181065
Accession Number
87N23980
Funding Number(s)
CONTRACT_GRANT: NAG5-749
CONTRACT_GRANT: NAG5-520
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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