GTOC12: Results from TheAntipodes

IF 2.7 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS
Roberto Armellin, Andrea Bellome, Xiaoyu Fu, Harry Holt, Cristina Parigini, Minduli Wijayatunga, Jack Yarndley
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引用次数: 0

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.

GTOC12: antipodes的结果
我们展示了由“TheAntipodes”团队在第12届全球轨迹优化竞赛(GTOC12)期间开发的解决方案。该方法的总体思路如下:(1)生成小行星子集;(2)利用束搜索构建链;(3)凸低推力轨迹优化;(4)人工优化交会时间;(5)选择最优解集。小行星子集的生成涉及一个启发式过程,以找到可能允许高分小行星链的小行星集。通过基于朗伯特转移的光束搜索,在每个子集内构建小行星序列“链”。低推力轨迹优化涉及到顺序凸规划(SCP)的使用,其中一个专门的公式在秒内找到每艘船的轨迹的质量最优控制。一旦找到可行的轨迹,在最优解的控制剖面的帮助下,人工精确地确定交会时间。然后将每艘船的单独解决方案放入一个池中,在该池中使用遗传算法提取使最终得分最大化的可行集。我们最终提交的解决方案以15,489分排名第五。
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来源期刊
Astrodynamics
Astrodynamics Engineering-Aerospace Engineering
CiteScore
6.90
自引率
34.40%
发文量
32
期刊介绍: Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.
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