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Research Article | Open Access

GTOC12: Results from TheAntipodes

Te Pūnaha Ātea — Space Institute, University of Auckland, Auckland 1010, New Zealand
Department of Aerospace Vehicles Design and Control, ISAE-Supaero, Toulouse 31400, France
Department of Mechanical and Aerospace Engineering, University of Liverpool, Liverpool L69 3BX, UK
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Abstract

We present the solution approach developed by the team "TheAntipodes" during the 12th edition of the Global Trajectory Optimization Competition (GTOC12). An overview of the approach is as follows: (1) generate asteroid subsets, (2) chain building with beam search, (3) convex low-thrust trajectory optimization, (4) manual refinement of rendezvous times, and (5) optimal solution set selection. The generation of asteroid subsets involves a heuristic process to find sets of asteroids that are likely to permit high-scoring asteroid chains. Asteroid sequences "chains" are built within each subset through a beam search based on Lambert transfers. Low-thrust trajectory optimization involves the use of sequential convex programming (SCP), where a specialized formulation finds the mass-optimal control for each ship's trajectory within seconds. Once a feasible trajectory has been found, the rendezvous times are manually refined with the aid of the control profile from the optimal solution. Each ship's individual solution is then placed into a pool where the feasible set that maximizes the final score is extracted using a genetic algorithm. Our final submitted solution placed fifth with a score of 15,489.

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Astrodynamics
Pages 55-75

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Cite this article:
Armellin R, Bellome A, Fu X, et al. GTOC12: Results from TheAntipodes. Astrodynamics, 2025, 9(1): 55-75. https://doi.org/10.1007/s42064-024-0219-3

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Received: 20 December 2023
Accepted: 06 May 2024
Published: 04 March 2025
© The Author(s) 2025

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