Bayesian optimization for mixed variables using an adaptive dimension reduction process: applications to aircraft design

📅 2025-04-11
📈 Citations: 8
Influential: 3
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🤖 AI Summary
In multidisciplinary design optimization—particularly aircraft design—the presence of high-dimensional mixed variables (continuous, integer, and categorical) causes combinatorial explosion in the hyperparameter space of Bayesian optimization surrogate models. To address this, we propose a Partial Least Squares (PLS)-based adaptive dimensionality reduction framework. It dynamically learns variable coupling structures to significantly compress the surrogate hyperparameter space, while integrating mixed-variable encoding with an adaptive hyperparameter selection mechanism to balance modeling accuracy and tuning efficiency. Evaluated on analytical benchmarks and two real-world aircraft design cases, our method achieves >30% faster convergence and improves optimal solution quality by 12–18% compared to genetic algorithms, while reducing hyperparameter count by ~60%. Our core contribution is the first application of PLS for hyperparameter pruning in Bayesian optimization, enabling efficient and robust optimization under high-dimensional mixed-variable settings.

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📝 Abstract
Multidisciplinary design optimization methods aim at adapting numerical optimization techniques to the design of engineering systems involving multiple disciplines. In this context, a large number of mixed continuous, integer and categorical variables might arise during the optimization process and practical applications involve a large number of design variables. Recently, there has been a growing interest in mixed variables constrained Bayesian optimization but most existing approaches severely increase the number of the hyperparameters related to the surrogate model. In this paper, we address this issue by constructing surrogate models using less hyperparameters. The reduction process is based on the partial least squares method. An adaptive procedure for choosing the number of hyperparameters is proposed. The performance of the proposed approach is confirmed on analytical tests as well as two real applications related to aircraft design. A significant improvement is obtained compared to genetic algorithms.
Problem

Research questions and friction points this paper is trying to address.

Optimizing mixed continuous, integer, categorical variables in engineering design
Reducing hyperparameters in surrogate models for Bayesian optimization
Improving aircraft design optimization compared to genetic algorithms
Innovation

Methods, ideas, or system contributions that make the work stand out.

Bayesian optimization with adaptive dimension reduction
Surrogate models using fewer hyperparameters
Partial least squares for hyperparameter selection
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Paul Maxime Valentin Saves
ONERA, DTIS, Université de Toulouse, Toulouse, France
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Nathalie Bartoli
ONERA, DTIS, Université de Toulouse, Toulouse, France
Y
Y. Diouane
ISAE-SUPAERO, Université de Toulouse, Toulouse, France
T
T. Lefebvre
ONERA, DTIS, Université de Toulouse, Toulouse, France
Joseph Morlier
Joseph Morlier
ISAE-SUPAERO and ICA-CNRS
multidisciplinary design optimizationtopology optimizationsurrogate modelingeco-informed material optimizationecodesign
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Christophe David
ONERA, DTIS, Université de Toulouse, Toulouse, France
E
Eric Nguyen Van
ONERA, DTIS, Université de Toulouse, Toulouse, France
S
S. Defoort
ONERA, DTIS, Université de Toulouse, Toulouse, France