基于月球飞掠的NRHO转移轨道重大机动故障恢复轨道搜索方案

Yuki Matsumoto, Ryo Nakamura, Toshinori Ikenaga, S. Ueda
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引用次数: 0

摘要

JAXA正在考虑为Gateway提供材料的HTV-X (HTV-XG)。作为从地球到近直线晕轨道(NRHO)的过渡轨道,Gateway将停留在那里,使用月球飞越的霍曼过境轨道正在考虑在名义情况下。该轨道上的三个主要机动是跨月注入(TLI),动力月球回旋(PLSB)和NRHO注入(NRHOI)。已经研究了TLI故障的恢复轨迹,但NRHOI和PLSB机动的恢复轨迹尚未研究。因此,本文重点研究了NRHOI或PLSB失效情况下的恢复轨迹规划。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Recovery Orbit Search Scheme for Major Maneuver Failure in NRHO Transfer Orbit Using Lunar Flyby
JAXA is considering the HTV-X for Gateway (HTV-XG) to supply materials to Gateway. As a transition orbit from Earth to the Near Rectilinear Halo Orbit (NRHO) where Gateway will stay, the Hohmann transit orbit using a lunar flyby is being considered in the nominal case. The three major maneuvers in this orbit are the Trans-Lunar Injection (TLI), Powered Lunar Swing-By (PLSB), and NRHO Injection (NRHOI). Recovery trajectories for TLI failure have been studied, but recovery trajectories for NRHOI and PLSB maneuvers have not been studied yet. Therefore, this paper focuses on recovery trajectory planning in case of NRHOI or PLSB failure.
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