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Can Simulation Credibility Be Improved Using Sensitivity Analysis to Understand Input Data Effects on Model Outcome?Model and simulation (MS) credibility is defined as, the quality to elicit belief or trust in MS results. NASA-STD-7009 [1] delineates eight components (Verification, Validation, Input Pedigree, Results Uncertainty, Results Robustness, Use History, MS Management, People Qualifications) that address quantifying model credibility, and provides guidance to the model developers, analysts, and end users for assessing the MS credibility. Of the eight characteristics, input pedigree, or the quality of the data used to develop model input parameters, governing functions, or initial conditions, can vary significantly. These data quality differences have varying consequences across the range of MS application. NASA-STD-7009 requires that the lowest input data quality be used to represent the entire set of input data when scoring the input pedigree credibility of the model. This requirement provides a conservative assessment of model inputs, and maximizes the communication of the potential level of risk of using model outputs. Unfortunately, in practice, this may result in overly pessimistic communication of the MS output, undermining the credibility of simulation predictions to decision makers. This presentation proposes an alternative assessment mechanism, utilizing results parameter robustness, also known as model input sensitivity, to improve the credibility scoring process for specific simulations.
Document ID
20160000202
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Myers, Jerry G.
(NASA Glenn Research Center Cleveland, OH United States)
Young, M.
(Wyle Labs, Inc. Aerospace Div. Dayton, OH, United States)
Goodenow, Debra A.
(NASA Glenn Research Center Cleveland, OH United States)
Keenan, A.
(Wyle Labs, Inc. Aerospace Div. Dayton, OH, United States)
Walton, M.
(Wyle Labs, Inc. Aerospace Div. Dayton, OH, United States)
Boley, L.
(Wyle Labs, Inc. Aerospace Div. Dayton, OH, United States)
Date Acquired
January 5, 2016
Publication Date
January 13, 2015
Subject Category
Mathematical And Computer Sciences (General)
Aerospace Medicine
Numerical Analysis
Report/Patent Number
GRC-E-DAA-TN20412
Meeting Information
Meeting: NASA HRP Investigator''s Workshop
Location: Galveston, Texas
Country: United States
Start Date: January 13, 2015
End Date: January 15, 2015
Sponsors: NASA Headquarters
Funding Number(s)
WBS: WBS 444543.01.02.10
CONTRACT_GRANT: NAS9-02078
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Credibility
Validation
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