Statistical Design of Thermal Protection System Using Physics-Informed Neural Network
Karthik Reddy Lyathakula, Aseem Muhammad, Sevki Cesmeci

TL;DR
This paper introduces a physics-informed neural network framework combined with sequential Monte Carlo sampling to efficiently perform uncertainty quantification and reliability analysis for thermal protection system design in space vehicles.
Contribution
It presents a novel approach integrating PINNs and SMC for rapid, accurate TPS parameter estimation under uncertainty, improving over traditional computational methods.
Findings
PINN accuracy comparable to traditional numerical solutions
Significant speed-up in TPS reliability analysis
Effective parameter distribution estimation satisfying reliability constraints
Abstract
Thermal protection systems (TPS) of space vehicles are designed computationally rather than experimentally. They are validated using ground experiments, but all aspects of the flight cannot be replicated on ground. This ground-to-flight mapping introduces uncertainties which need to be accounted for while designing any thermal protection system. Thus, precise computational models along with uncertainty quantification in the models are required to design the TPS. The focus of this study is to estimate the thermal material parameters of TPS based on the target reliability requirements using statistical methods. To perform uncertainty quantification (UQ) of a system, a simulated model of the system needs to be solved many times on statistical samples, increasing the computational time and cost of the overall process. A physics-informed neural network (PINN) model is used in the analysis…
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Taxonomy
TopicsAdvanced Sensor and Control Systems · Engineering Applied Research
