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16 - 21 June 2024
Yokohama, Japan
Conference 13099 > Paper 13099-88
Paper 13099-88

Sensitivity analysis of coupled variables in integrated STOP models

17 June 2024 • 17:30 - 19:00 Japan Standard Time | Room G5, North - 1F

Abstract

The computational complexity of integrated structural-thermal-optical performance models, particularly for one-of-a-kind telescope missions, often limits the maximum feasible number of analysis cycles. Applications requiring a large number of model evaluations, such as uncertainty quantification and sensitivity analysis, can become infeasible if the number of required iterations for the analysis exceeds the allocated computation time or budget. Another major obstacle to the sensitivity analysis of integrated models is the dependence between variables, as correlation between the variables changes the contribution they have on the variance in output model predictions. This paper presents a multifidelity integrated modeling methodology that incorporates both high-fidelity and low-fidelity models to reduce the model’s computational cost while retaining sufficient accuracy for sensitivity analysis. Additionally, an estimation of the closed sensitivity indices is presented for the fully integrated model, taking into account the dependence between variables in structural-thermal-optical performance models.

Presenter

Rosemary K. Davidson
Massachusetts Institute of Technology (United States)
Rosemary is currently a PhD candidate in the Space Systems Lab at the Massachusetts Institute of Technology. Her research focuses on uncertainty quantification and sensitivity analysis of integrated models, particularly when applied to early design phases for telescope missions. Rosemary is also a founding member of the Women of Aeronautics and Astronautics committee within AIAA.
Presenter/Author
Rosemary K. Davidson
Massachusetts Institute of Technology (United States)
Author
NASA Goddard Space Flight Ctr. (United States)
Author
Massachusetts Institute of Technology (United States)