MLJan 18, 2018

Upgrading from Gaussian Processes to Student's-T Processes

arXiv:1801.06147v143 citations
Originality Incremental advance
AI Analysis

This work addresses robustness issues in optimization for aerospace engineering, though it appears incremental as it generalizes an existing method.

The paper tackles the limitations of Gaussian processes in Bayesian optimization for aerospace design, such as handling outliers and posterior variance dependence, by introducing Student's-T processes, which show improved performance on test problems and an aerostructural design application.

Gaussian process priors are commonly used in aerospace design for performing Bayesian optimization. Nonetheless, Gaussian processes suffer two significant drawbacks: outliers are a priori assumed unlikely, and the posterior variance conditioned on observed data depends only on the locations of those data, not the associated sample values. Student's-T processes are a generalization of Gaussian processes, founded on the Student's-T distribution instead of the Gaussian distribution. Student's-T processes maintain the primary advantages of Gaussian processes (kernel function, analytic update rule) with additional benefits beyond Gaussian processes. The Student's-T distribution has higher Kurtosis than a Gaussian distribution and so outliers are much more likely, and the posterior variance increases or decreases depending on the variance of observed data sample values. Here, we describe Student's-T processes, and discuss their advantages in the context of aerospace optimization. We show how to construct a Student's-T process using a kernel function and how to update the process given new samples. We provide a clear derivation of optimization-relevant quantities such as expected improvement, and contrast with the related computations for Gaussian processes. Finally, we compare the performance of Student's-T processes against Gaussian process on canonical test problems in Bayesian optimization, and apply the Student's-T process to the optimization of an aerostructural design problem.

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