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Planetary Defense From Space: Part 1-Keplerian Theory

机译:来自太空的行星防御:第1部分:基普勒理论

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摘要

A system of two space bases housing missiles is proposed to achieve the Planetary Defense of the Earth against dangerous asteroids and comets. We show that the layout of the Earth-Moon system with the five relevant Lagrangian (or libration) points in space leads naturally to only one, unmistakable location of these two space bases within the sphere of influence of the Earth. These locations are at the two Lagrangian points L1 (in between the Earth and the Moon) and L3 (in the direction opposite to the Moon from the Earth). We show that placing bases of missiles at L1 and L3 would cause those missiles to deflect the trajectory of asteroids by hitting them orthogonally to their impact trajectory toward the Earth, so as to maximize their deflection. We show that the confocal conies are the best class of trajectories fulfilling this orthogonal deflection requirement. An additional remark is that the theory developed in this paper is just a beginning of a larger set of future research work. In fact, while in this paper we only develop the Keplerian analytical theory of the Optimal Planetary Defense achievable from the Earth-Moon Lagrangian points L1 and L3, much more sophisticated analytical refinements would be needed to: (1) Take into account many perturbation forces of all kinds acting on both the asteroids and missiles shot from L1 and L3; (2) add more (non-optimal) trajectories of missiles shot from either the Lagrangian points L4 and L5 of the Earth-Moon system or from the surface of the Moon itself; (3) encompass the full range of missiles currently available to the US (and possibly other countries) so as to really see "which asteroids could be diverted by which missiles", even in the very simplified scheme outlined here. Outlined for the first time in February 2002, our Confocal Planetary Defense concept is a Keplerian Theory that proved simple enough to catch the attention of scholars, representatives of the US Military and popular writers. These developments could possibly mark the beginning of an "all embracing" mathematical vision of Planetary Defense beyond all learned activities, dramatic movies and unknown military plans covered by secret.
机译:提出了一个由两个装有导弹的空间基地组成的系统,以实现对危险小行星和彗星的地球行星防御。我们表明,在空间中具有五个相关的拉格朗日(或解放)点的地月系统的布局自然会导致这两个空间基在地球影响范围内只有一个明确的位置。这些位置位于两个拉格朗日点L1(在地球和月球之间)和L3(在与地球相对的月亮方向上)。我们表明,将导弹的基地放置在L1和L3处会导致这些导弹偏转小行星的轨迹,方法是使其垂直撞击地球,从而使其偏转最大化。我们证明了共聚焦圆锥是满足这种正交偏转要求的最好的轨迹类别。另一个要点是,本文开发的理论只是未来大量研究工作的开端。实际上,尽管在本文中,我们仅开发了从月球拉格朗日点L1和L3可获得的最佳行星防御的开普勒分析理论,但仍需要进行更复杂的分析改进:(​​1)考虑到许多微扰力对L1和L3发射的小行星和导弹都起作用的种类; (2)增加从地月系统的拉格朗日点L4和L5或从月球表面发射的更多(非最佳)导弹轨迹; (3)涵盖了美国(以及其他国家)目前可获得的全部导弹,即使在这里概述的非常简化的方案中,也能真正看到“哪些小行星可以被哪些导弹转移”。我们的共焦行星防御概念是2002年2月首次概述的,它是一种开普勒理论,事实证明它很简单,足以引起学者,美国军事代表和大众作家的注意。这些发展可能标志着对行星防御的“全盘拥抱”数学愿景的开始,超越了所有学到的活动,戏剧电影和秘密所涵盖的未知军事计划。

著录项

  • 来源
    《Acta astronautica》 |2004年第12期|p.991-1006|共16页
  • 作者

    Claudio Maccone;

  • 作者单位

    Via Martorelli 43, I-10155 Torino (TO), Italy;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航天(宇宙航行);
  • 关键词

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