Two-Level Approach for Simultaneous Component Assignment and Layout Optimization with Applications to Spacecraft Optimal Layout

Optimal layout problems consist in positioning a given number of components in order to minimize an objective function while satisfying geometrical or functional constraints. Such kinds of problems appear in the design process of aerospace systems such as satellite or spacecraft design. These problems are NP-hard, highly constrained and dimensional. This paper describes a two-stage algorithm combining a genetic algorithm and a quasi-physical approach based on a virtual-force system in order to solve multi-container optimal layout problems such as satellite modules. In the proposed approach, a genetic algorithm assigns the components to the containers while a quasi-physical algorithm based on a virtual-force system is developed for positioning the components in the assigned containers. The proposed algorithm is experimented and validated on the satellite module layout problem benchmark. Its global performance is compared with previous algorithms from the literature.

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Publication Details

Journal
Applied Sciences
Published
2024-09-10
DOI
https://doi.org/10.3390/app14188120
Primary Topic
Advanced Manufacturing and Logistics Optimization
Type
article
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article

Two-Level Approach for Simultaneous Component Assignment and Layout Optimization with Applications to Spacecraft Optimal Layout

Mathieu Balesdent, Juliette Gamot, Arnault Tremolet, Nouredine Melab et al.
Applied Sciences
Advanced Manufacturing and Logistics Optimization
article

Two-Level Approach for Simultaneous Component Assignment and Layout Optimization with Applications to Spacecraft Optimal Layout

Mathieu Balesdent, Juliette Gamot, Arnault Tremolet, Nouredine Melab, Romain Wuilbercq
article en

Abstract

Optimal layout problems consist in positioning a given number of components in order to minimize an objective function while satisfying geometrical or functional constraints. Such kinds of problems appear in the design process of aerospace systems such as satellite or spacecraft design. These problems are NP-hard, highly constrained and dimensional. This paper describes a two-stage algorithm combining a genetic algorithm and a quasi-physical approach based on a virtual-force system in order to solve multi-container optimal layout problems such as satellite modules. In the proposed approach, a genetic algorithm assigns the components to the containers while a quasi-physical algorithm based on a virtual-force system is developed for positioning the components in the assigned containers. The proposed algorithm is experimented and validated on the satellite module layout problem benchmark. Its global performance is compared with previous algorithms from the literature.

Applied SciencesVol. 14(18)
Centre National de la Recherche Scientifique (FR), Université de Lille (FR), Université Paris-Saclay (FR)
Openalex Percentile: Top 79%
Advanced Manufacturing and Logistics Optimization
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