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Selection of Thermal Worst-Case Orbits via Modified Efficient Global OptimizationEfficient Global Optimization (EGO) was used to select orbits with worst-case hot and cold thermal environments for the Stratospheric Aerosol and Gas Experiment (SAGE) III. The SAGE III system thermal model changed substantially since the previous selection of worst-case orbits (which did not use the EGO method), so the selections were revised to ensure the worst cases are being captured. The EGO method consists of first conducting an initial set of parametric runs, generated with a space-filling Design of Experiments (DoE) method, then fitting a surrogate model to the data and searching for points of maximum Expected Improvement (EI) to conduct additional runs. The general EGO method was modified by using a multi-start optimizer to identify multiple new test points at each iteration. This modification facilitates parallel computing and decreases the burden of user interaction when the optimizer code is not integrated with the model. Thermal worst-case orbits for SAGE III were successfully identified and shown by direct comparison to be more severe than those identified in the previous selection. The EGO method is a useful tool for this application and can result in computational savings if the initial Design of Experiments (DoE) is selected appropriately.
Document ID
20140011302
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Moeller, Timothy M.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Wilhite, Alan W.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Liles, Kaitlin A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2014
Publication Date
March 1, 2014
Subject Category
Space Sciences (General)
Report/Patent Number
NF1676L-18151
L-20365
NASA/TM-2014-218182
Report Number: NF1676L-18151
Report Number: L-20365
Report Number: NASA/TM-2014-218182
Funding Number(s)
WBS: WBS 857865.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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