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An indirect method for numerical optimization using the Kreisselmeir-Steinhauser functionA technique is described for converting a constrained optimization problem into an unconstrained problem. The technique transforms one of more objective functions into reduced objective functions, which are analogous to goal constraints used in the goal programming method. These reduced objective functions are appended to the set of constraints and an envelope of the entire function set is computed using the Kreisselmeir-Steinhauser function. This envelope function is then searched for an unconstrained minimum. The technique may be categorized as a SUMT algorithm. Advantages of this approach are the use of unconstrained optimization methods to find a constrained minimum without the draw down factor typical of penalty function methods, and that the technique may be started from the feasible or infeasible design space. In multiobjective applications, the approach has the advantage of locating a compromise minimum design without the need to optimize for each individual objective function separately.
Document ID
19890007408
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wrenn, Gregory A.
(Planning Research Corp. Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Publication Information
Publisher: NASA
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-4220
NAS 1.26:4220
Accession Number
89N16779
Funding Number(s)
CONTRACT_GRANT: NAS1-18000
PROJECT: RTOP 506-43-41-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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