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Strategies for Automation of Model Tuning in Multifidelity Trajectory Uncertainty PropagationMulti-model Monte Carlo methods are efficient strategies to perform forward uncertainty quantification studies in entry, descent, and landing (EDL) applications. These multi-model methods are based on the classical Monte Carlo estimator, but fuse predictions from several low-fidelity models to obtain estimators with greater precision given a prescribed computational budget. The effectiveness of these approaches relies on the magnitudes of correlations between the low-fidelity models and the high-fidelity model, as well as the relative computational costs of all models. Identifying and exploiting the best trade-off between correlation and cost, which ultimately depends on the selection of hyperparameters in the low-fidelity models, is a task often performed by hand or simply inspired by the deterministic understanding available for a specific application. This work extends a preliminary effort,
Document ID
20220018522
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Marten Thompson
(University of Minnesota Minneapolis, Minnesota, United States)
Gianluca Geraci
(Sandia National Laboratories Albuquerque, New Mexico, United States)
Geoffrey F Bomarito
(Langley Research Center Hampton, Virginia, United States)
James E Warner
(Langley Research Center Hampton, Virginia, United States)
Patrick E Leser
(Langley Research Center Hampton, Virginia, United States)
William P Leser
(Langley Research Center Hampton, Virginia, United States)
Michael S Eldred
(Sandia National Laboratories Albuquerque, New Mexico, United States)
John D Jakeman
(Sandia National Laboratories Albuquerque, New Mexico, United States)
Alex A Gorodetsky
(University of Michigan–Ann Arbor Ann Arbor, Michigan, United States)
Date Acquired
December 6, 2022
Subject Category
Astrodynamics
Meeting Information
Meeting: 2023 AIAA SciTech
Location: National Harbor, MD
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 335803.04.22.23.10.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
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