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Integration of Uncertainty Quantification in a Model-Based Systems Analysis and Engineering FrameworkThis paper presents a technical approach to improve the confidence in the systems analysis process by integrating Uncertainty Quantification (UQ) techniques within a Model-Based Systems Analysis and Engineering (MBSA&E) framework. The MBSA&E architecture uses system models and multidisciplinary analytical solutions as central artifacts for system design and analysis. The integration of UQ enables engineers to assess and mitigate uncertainties associated with a system model, design parameters, and constraint inputs, leading to more complete design studies and further informed decision-making processes. The proposed approach leverages the strengths of MBSA&E and extends it with a UQ methodology to quantify uncertainties in the input parameters and to trace the uncertainties as they propagate throughout the system model. To demonstrate the effectiveness of an integrated MBSA&E-UQ approach, a case study involving a simplified analysis of a Transonic Truss-Braced Wing (TTBW) concept vehicle is performed. This integration enables a more comprehensive evaluation of system performance and behavior under uncertainty and a more robust approach for system design and analysis. Lastly, the paper addresses the challenges and considerations associated with integrating UQ into an MBSA&E framework.
Document ID
20240009195
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Bijan Fazal
(Langley Research Center Hampton, Virginia, United States)
Joanna Schmidt
(Langley Research Center Hampton, United States)
Ben Phillips
(Langley Research Center Hampton, Virginia, United States)
Irian Ordaz
(Langley Research Center Hampton, Virginia, United States)
Kenneth Moore
(Banner Quality Management Friendswood, Texas, United States)
Date Acquired
July 18, 2024
Subject Category
Aeronautics (General)
Computer Programming and Software
Meeting Information
Meeting: AIAA Aviation Forum
Location: Las Vegas, NV
Country: US
Start Date: July 29, 2024
End Date: August 2, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 081876.02.07.30.10.01
WBS: 109492.02.07.06.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
systems analysis
systems engineering
model-based systems engineering
multidisciplinary design analysis and optimization
uncertainty quantification
truss-braced transonic wing
model-based systems analysis and engineering
model-based systems analysis
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