@article{XU2026, 
author = {Hang XU and Bin SONG and Lujiang LIU and Xinglong LI and Qiufan YUAN},
title = {Fast replanning method for large-scale on-orbit servicing missions},
year = {2026},
journal = {Acta Aeronautica et Astronautica Sinica},
volume = {47},
number = {14},
keywords = {on-orbit service, Lambert transfer, re-planning, online optimization, beam search, attention model},
url = {https://www.sciopen.com/article/10.7527/S1000-6893.2025.32728},
doi = {10.7527/S1000-6893.2025.32728},
abstract = {To meet the requirements of large-scale on-orbit service mission planning, existing research is usually confined to static scenarios, making it difficult to tackle the invalidation of initial plans caused by unexpected events such as spacecraft failures and task changes. This calls for on-the-fly replanning with flexible Lambert transfers. However, this mission is a mixed-integer programming problem involving three nested optimization layers: trajectory planning, sequence planning, and task assignment. Current strategies involve extensive iterative computations, especially for Lambert transfers that require numerical iterative solutions, which severely limits their practical engineering applications. To address this challenge, this paper proposes an efficient algorithmic framework. First, for the underlying trajectory planning and sequence planning problems, deep neural networks and attention models are adopted respectively to replace the online optimization iteration process, enabling rapid solutions. Second, for the upper-layer task assignment problem, a Beam Pre-search and Neighborhood Optimization Algorithm (BPNOA) based on historical preplans is proposed. By integrating mechanisms including target assignment state labeling, coarse screening of suitable spacecraft based on combined orbit transfer strategies, pre-plan adjustment using beam search and auction strategies, and local optimization, the proposed framework realizes an efficient solution process characterized by “fast initial optimization followed by fine-tuning”. Finally, using real orbital data from the CelesTrak website, comparative experiments with genetic algorithms demonstrate that in small-scale scenario tests, the proposed method exhibits an average convergence efficiency over 150 times higher; in 99 Monte Carlo tests of large-scale scenarios, with the same calculations, the average optimization result of the proposed method is improved by 71%, and the standard deviation of multiple solutions is reduced by 84.1%. The convergence is better and more robust. The results verify the effectiveness of the new method, which can significantly improve the efficiency of task replanning and meet the real-time requirements of future applications.}
}