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Full Length Article | Open Access

Mixed integer programming modeling for the satellite three-dimensional component assignment and layout optimization problem

Yufeng XIAa,b,cXianqi CHENb,c( )Zhijia LIUdWeien ZHOUb,cWen YAOb,c ( )Zhongneng ZHANGa,b,c
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
Defense Innovation Institute, Chinese Academy of Military Science, Beijing 100071, China
Intelligent Game and Decision Laboratory, Beijing 100071, China
DFH Satellite Co., Ltd., Beijing 100094, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Satellite Component Layout Optimization (SCLO) is crucial in satellite system design. This paper proposes a novel Satellite Three-Dimensional Component Assignment and Layout Optimization (3D-SCALO) problem tailored to engineering requirements, aiming to optimize satellite heat dissipation while considering constraints on static stability, 3D geometric relationships between components, and special component positions. The 3D-SCALO problem is a challenging bilevel combinatorial optimization task, involving the optimization of discrete component assignment variables in the outer layer and continuous component position variables in the inner layer, with both influencing each other. To address this issue, first, a Mixed Integer Programming (MIP) model is proposed, which reformulates the original bilevel problem into a single-level optimization problem, enabling the exploration of a more comprehensive optimization space while avoiding iterative nested optimization. Then, to model the 3D geometric relationships between components within the MIP framework, a linearized 3D Phi-function method is proposed, which handles non-overlapping and safety distance constraints between cuboid components in an explicit and effective way. Subsequently, the Finite-Rectangle Method (FRM) is proposed to manage 3D geometric constraints for complex-shaped components by approximating them with a finite set of cuboids, extending the applicability of the geometric modeling approach. Finally, the feasibility and effectiveness of the proposed MIP model are demonstrated through two numerical examples and a real-world engineering case, which confirms its suitability for complex-shaped components and real engineering applications.

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Chinese Journal of Aeronautics

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Cite this article:
XIA Y, CHEN X, LIU Z, et al. Mixed integer programming modeling for the satellite three-dimensional component assignment and layout optimization problem. Chinese Journal of Aeronautics, 2025, 38(6). https://doi.org/10.1016/j.cja.2025.103415

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Received: 28 May 2024
Revised: 05 September 2024
Accepted: 06 November 2024
Published: 22 January 2025
© 2025 The Authors. Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).