NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Improving Multi-Model Trajectory Simulation Estimators using Model Selection and TuningMulti-model Monte Carlo methods have been demonstrated to be an efficient and accurate alternative to standard Monte Carlo (MC) in the model-based propagation of uncertainty in entry, descent, and landing (EDL) applications. These multi-model MC methods fuse predictions from low-fidelity models with the high-fidelity EDL model of interest to produce unbiased statistics with a fraction of the computational cost. The accuracy and efficiency of the multi-model MC methods are dependent upon the magnitude of correlations of the low-fidelity models with the high-fidelity model, but also upon the correlation amongst the low-fidelity models, and their relative computational cost. Because of this layer of complexity, the question of how to optimally select the set of low-fidelity models has remained open. In this work, methods for optimal model construction and tuning are investigated as a means to increase the speed and precision of trajectory simulation for EDL. Specifically, the focus is on the inclusion of low-fidelity model tuning within the sample allocation optimization that accompanies multi-model MC methods.
Preliminary results indicate that low-fidelity model tuning can significantly improve efficiency and precision of trajectory simulations and provide an increased edge to multi-model MC methods when compared to standard MC. The challenges and potential benefits to exploring a fully iterative and comprehensive optimization strategy in future work are highlighted.
Document ID
20210025248
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Geoffrey Bomarito
(Langley Research Center Hampton, Virginia, United States)
Gianluca Geraci
(Sandia National Laboratories Albuquerque, New Mexico, United States)
James Warner
(Langley Research Center Hampton, Virginia, United States)
Patrick Leser
(Langley Research Center Hampton, Virginia, United States)
Paul Leser
(Langley Research Center Hampton, Virginia, United States)
Michael Eldred
(Sandia National Laboratories Albuquerque, New Mexico, United States)
John Jakeman
(Sandia National Laboratories Albuquerque, New Mexico, United States)
Alex Gorodetsky
(University of Michigan–Ann Arbor Ann Arbor, Michigan, United States)
Date Acquired
December 1, 2021
Subject Category
Numerical Analysis
Meeting Information
Meeting: AIAA Scitech
Location: San Diego, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
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 Technical Management
Keywords
uncertainty quantification
trajectory simulation
multifidelity
No Preview Available