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In this paper the Lambert relative motion problem of elliptical orbit in near-range approaching phase for spacecraft rendezvous and docking is studied. Based on the relative motion kinetic equations of the elliptical orbit, the velocity increment of Lambert relative motion transfer method is calculated, and the general features of Lambert relative motion of elliptical orbit in near-range approaching phase are summarized.

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Research for Relative Motion Lambert Theory of Elliptical Orbit

  • 会议论文

  • 发表日期：

    2025年

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  • Xu Limin,
  • Chen Yu,
  • Zhang Hongliang,
  • Zhai Zhipeng

摘要

In this paper the Lambert relative motion problem of elliptical orbit in near-range approaching phase for spacecraft rendezvous and docking is studied. Based on the relative motion kinetic equations of the elliptical orbit, the velocity increment of Lambert relative motion transfer method is calculated, and the general features of Lambert relative motion of elliptical orbit in near-range approaching phase are summarized.