An Investigation of Surrogate-Assisted, Gradient-Based Methods for Stellarator Breeder Geometry Optimization

The stellarator blanket design problem is characterized by many degrees of freedom in which the designer is tasked with fitting a series of layered components between the plasma and the magnets, usually resulting in components of a nonuniform geometry to meet the performance goals. For such a problem, numerical optimization methods are well suited to efficiently and autonomously explore the design space and find an optimized design. This preliminary study investigates the application of surrogate-assisted, gradient-based methods to stellarator breeder geometry design.The investigation includes the development of an accurate surrogate model to predict design point gradients and its incorporation into gradient-based algorithms. The developed methodology is successfully demonstrated for the WISTELL-D stellarator configuration, reducing blanket material costs below that of a reference while meeting a target tritium breeding ratio, and a detailed analysis of the optimization runs is presented. Future work will expand this methodology to incorporate control of the shielding components and shielding-relevant metrics.

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Publication Details

Journal
Fusion Science & Technology
Published
2026-09-04
DOI
https://doi.org/10.1080/15361055.2026.2721695
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
0.00
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article

An Investigation of Surrogate-Assisted, Gradient-Based Methods for Stellarator Breeder Geometry Optimization

Paul P.H. Wilson, Connor A. Moreno
Fusion Science & Technology
Spacecraft Dynamics and Control
article

An Investigation of Surrogate-Assisted, Gradient-Based Methods for Stellarator Breeder Geometry Optimization

Paul P.H. Wilson, Connor A. Moreno
article en

Abstract

The stellarator blanket design problem is characterized by many degrees of freedom in which the designer is tasked with fitting a series of layered components between the plasma and the magnets, usually resulting in components of a nonuniform geometry to meet the performance goals. For such a problem, numerical optimization methods are well suited to efficiently and autonomously explore the design space and find an optimized design. This preliminary study investigates the application of surrogate-assisted, gradient-based methods to stellarator breeder geometry design.The investigation includes the development of an accurate surrogate model to predict design point gradients and its incorporation into gradient-based algorithms. The developed methodology is successfully demonstrated for the WISTELL-D stellarator configuration, reducing blanket material costs below that of a reference while meeting a target tritium breeding ratio, and a detailed analysis of the optimization runs is presented. Future work will expand this methodology to incorporate control of the shielding components and shielding-relevant metrics.

Fusion Science & Technology
University of Wisconsin–Madison (US)
Climate action
Openalex Percentile: Top 7%
Spacecraft Dynamics and Control
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An Investigation of Surrogate-Assisted, Gradient-Based Methods for Stellarator Breeder Geometry Optimization — Paul P.H. Wilson, Connor A. Moreno · Fusion Science & Technology (2026) | TGRS Research Map | TGRS