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Structural tailoring and feedback control synthesis - An interdisciplinary approachStructural tailoring provides an attractive method to optimize the performance of actively controlled space structures. However, the simultaneous optimization of control gains and structural properties often becomes prohibitively expensive for large systems and physical insight is often lost in the resulting control law. This paper presents a method for optimization of the closed loop structural system using only structural tailoring. Optimal Linear Quadratic Regulator (LQR) control theory is used with weighting matrices chosen based on physical considerations. The LQR control law depends only on two scalar gains and the structural properties. Hence, the closed loop-performance can be expressed in terms of the structural parameters. Results are given for a beam and a truss-beam to show the simplicity of the method and the importance of structural tailoring to increase dynamic performance and to reduce the control effort.
Document ID
19880044950
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Belvin, W. Keith
(NASA Langley Research Center Hampton, VA, United States)
Park, K. C.
(Colorado, University Boulder, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Cybernetics
Report/Patent Number
AIAA PAPER 88-2206
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference
Location: Williamsburg, VA
Country: United States
Start Date: April 18, 1988
End Date: April 20, 1988
Sponsors: Structures
Accession Number
88A32177
Funding Number(s)
CONTRACT_GRANT: F49620-87-C-0074
Distribution Limits
Public
Copyright
Other

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