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Simultaneous structural and control optimization via linear quadratic regulator eigenstructure assignmentA method for simultaneous structural and control design of large flexible space structures (LFSS) to reduce vibration generated by disturbances is presented. Desired natural frequencies and damping ratios for the closed loop system are achieved by using a combination of linear quadratic regulator (LQR) synthesis and numerical optimization techniques. The state and control weighing matrices (Q and R) are expressed in terms of structural parameters such as mass and stiffness. The design parameters are selected by numerical optimization so as to minimize the weight of the structure and to achieve the desired closed-loop eigenvalues. An illustrative example of the design of a two bar truss is presented.
Document ID
19880004240
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Becus, G. A.
(Cincinnati Univ. OH, United States)
Lui, C. Y.
(Cincinnati Univ. OH, United States)
Venkayya, V. B.
(Cincinnati Univ. OH, United States)
Tischler, V. A.
(Air Force Wright Aeronautical Labs. Wright-Patterson AFB, Ohio., United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA-Marshall Space Flight Center, The 58th Shock and Vibration Symposium, Volume 1
Subject Category
Structural Mechanics
Accession Number
88N13622
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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