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郝志鑫, 郑建华, 李明涛. 黄道面内多目标小行星飞越探测任务轨道优化设计[J]. 深空探测学报(中英文), 2022, 9(4): 373-381. DOI: 10.15982/j.issn.2096-9287.2022.20210143
引用本文: 郝志鑫, 郑建华, 李明涛. 黄道面内多目标小行星飞越探测任务轨道优化设计[J]. 深空探测学报(中英文), 2022, 9(4): 373-381. DOI: 10.15982/j.issn.2096-9287.2022.20210143
HAO Zhixin, ZHENG Jianhua, LI Mingtao. Trajectory Optimization Design for Multiple-Target Asteroid Flyby Mission in Ecliptic Plane[J]. Journal of Deep Space Exploration, 2022, 9(4): 373-381. DOI: 10.15982/j.issn.2096-9287.2022.20210143
Citation: HAO Zhixin, ZHENG Jianhua, LI Mingtao. Trajectory Optimization Design for Multiple-Target Asteroid Flyby Mission in Ecliptic Plane[J]. Journal of Deep Space Exploration, 2022, 9(4): 373-381. DOI: 10.15982/j.issn.2096-9287.2022.20210143

黄道面内多目标小行星飞越探测任务轨道优化设计

Trajectory Optimization Design for Multiple-Target Asteroid Flyby Mission in Ecliptic Plane

  • 摘要: 近距离飞越小行星可获取小行星的表面图像、测量小行星的光谱、反演小行星物理化学性质。对潜在威胁小行星实施多目标飞越探测任务进行轨道优化设计,分析了潜在威胁小行星穿越黄道面时刻与位置分布,以小行星穿越黄道面时刻作为探测器飞越小行星的时刻,通过波束选择树搜索算法优化求解序贯飞越序列,建立了一种快速有效求解小行星序贯飞越任务轨道的优化方法模型。仿真结果表明,2024—2028年发射的小行星探测器可在黄道面内飞越探测至少18颗潜在威胁小行星,2027年9月发射窗口在10 a任务周期内可飞越21颗潜在威胁小行星。

     

    Abstract: Closely flying by asteroids can help to capture asteroid surface images, measure asteroid spectra, and obtain physical and chemical properties of asteroids. In particular, flying by multiple asteroids with potential hazards to the earth in one mission will significantly improve the understanding of the characteristics of potentially hazardous asteroids, and it is also of great significance to asteroid defense missions. In this paper, the trajectory of the multiple asteroid flyby mission of potentially hazardous asteroids was optimized. Firstly, the time and position distribution of asteroids passing through the ecliptic plane were analyzed, and the basic strategy of asteroids flyby in the ecliptic was determined. The time of asteroids crossing the ecliptic was taken as the time of asteroids’ flyby. Secondly, the sequential flyby sequence was optimized via beam selection tree search algorithm, and an optimization model for fast and effective solution of asteroid sequential flyby mission trajectory was established. Simulation results show that missions launched from 2024 to 2028 can fly by at least 18 potentially hazardous asteroids, especially the launch window in September 2027, which can fly by 21 potentially hazardous asteroids within a ten-year mission duration.

     

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