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在多体系统中,对航天器轨迹设计的运动原始方法
Thomas R Smith1, Natasha Bosanac1
1Colorado Center for Astrodynamics Research, Smead Department of Aerospace Engineering Sciences, University of Colorado Boulder, 3775 Discovery Dr., Boulder, CO 80303 USA.
概括
这项研究引入了一种新的框架,用于在多体系统中快速设计航天器轨迹的运动原体. 这种方法有效地产生了在 libration 点轨道之间多样化的转移轨迹.
科学领域:
- 天体动力学是指天体动力学.
- 机器人技术 机器人技术 机器人技术
- 太空飞船轨道设计设计
背景情况:
- 在 cislunar 和多体环境中增加航天器操作需要更快的轨道设计.
- 机器人利用运动原体来高效地构建复杂的路径.
研究的目的:
- 开发一个框架,用于在多体引力系统中快速和明智地设计航天器轨迹.
- 为了利用运动原体来构建复杂的航天器轨迹.
主要方法:
- 通过聚类生成运动原始体 (周期轨道,多重体) 来总结相位空间.
- 构建和搜索运动原始的图形,以进行初始轨迹猜测.
- 使用多目标受约束优化和拼接计算的连续转移.
主要成果:
- 通过在地球-月球 libration 点轨道之间创建多样化的转移来演示框架.
- 通过冲动机动成功生成了几何上不同的转移轨迹.
结论:
- 运动原始框架允许在复杂的引力环境中快速和知情地设计轨迹.
- 这种方法对于产生航天器转移的初步猜测是有效的,特别是在 libration point 轨道之间.
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