NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
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
19890024310
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baz, A.
(Catholic Univ. of America Washington, DC, United States)
Poh, S.
(Catholic University of America, Washington, DC, United States)
Studer, P.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Cybernetics
Meeting Information
Meeting: VPI&SU/AIAA Symposium
Location: Blacksburg, VA
Country: United States
Start Date: June 29, 1987
End Date: July 1, 1987
Accession Number
89A11681
Funding Number(s)
CONTRACT_GRANT: NAG5-520
CONTRACT_GRANT: NAG5-749
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available