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A sequential linear optimization approach for controller designA linear optimization approach with a simple real arithmetic algorithm is presented for reliable controller design and vibration suppression of flexible structures. Using first order sensitivity of the system eigenvalues with respect to the design parameters in conjunction with a continuation procedure, the method converts a nonlinear optimization problem into a maximization problem with linear inequality constraints. The method of linear programming is then applied to solve the converted linear optimization problem. The general efficiency of the linear programming approach allows the method to handle structural optimization problems with a large number of inequality constraints on the design vector. The method is demonstrated using a truss beam finite element model for the optimal sizing and placement of active/passive-structural members for damping augmentation. Results using both the sequential linear optimization approach and nonlinear optimization are presented and compared. The insensitivity to initial conditions of the linear optimization approach is also demonstrated.
Document ID
19850063802
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Horta, L. G.
(NASA Langley Research Center Hampton, VA, United States)
Juang, J.-N.
(NASA Langley Research Center Hampton, VA, United States)
Junkins, J. L.
(Virginia Polytechnic Institute, Blacksburg, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 85-1971
Meeting Information
Meeting: Guidance, Navigation and Control Conference
Location: Snowmass, CO
Start Date: August 19, 1985
End Date: August 21, 1985
Accession Number
85A45953
Distribution Limits
Public
Copyright
Other

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