NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Optimization Based Efficiencies in First Order Reliability AnalysisThis paper develops a method for updating the gradient vector of the limit state function in reliability analysis using Broyden's rank one updating technique. In problems that use commercial code as a black box, the gradient calculations are usually done using a finite difference approach, which becomes very expensive for large system models. The proposed method replaces the finite difference gradient calculations in a standard first order reliability method (FORM) with Broyden's Quasi-Newton technique. The resulting algorithm of Broyden updates within a FORM framework (BFORM) is used to run several example problems, and the results compared to standard FORM results. It is found that BFORM typically requires fewer functional evaluations that FORM to converge to the same answer.
Document ID
20030062103
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Peck, Jeffrey A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Mahadevan, Sankaran
(Vanderbilt Univ. Nashville, TN, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Numerical Analysis
Meeting Information
Meeting: 44th American Institute of Aeronautics and Astronautics (AIAA) Structures, Structural Dynamics, and Materials Conference
Location: Norfolk, VA
Country: United States
Start Date: April 7, 2003
End Date: April 10, 2003
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
Document Inquiry

Available Downloads

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