TY - JOUR
T1 - Analysis of Transfer Trajectories in Cislunar Space Using Sequences of Lobe Dynamics
AU - Hiraiwa, Naoki
AU - Bando, Mai
AU - Hokamoto, Shinji
N1 - Publisher Copyright:
Copyright © 2023 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2023
Y1 - 2023
N2 - The Gateway will be constructed as a staging point for exploring cislunar space in the Artemis program. For the maintenance of this platform, uncrewed cargo transport is planned by JAXA. To efficiently conduct cargo transport, this study proposes a novel methodology to design low-energy chaotic transfers based on lobe dynamics in the planar circular restricted three-body problem (CR3BP). Lobe dynamics focuses on the " lobe, " the region determined by stable and unstable manifolds of a resonant orbit, and can reveal phase space transport of chaotic trajectories. In general, lobe dynamics of one resonant orbit can transfer a spacecraft only around the tori related to the resonant orbit in concern. The proposed method combines lobe dynamics of various resonant orbits to make a desired transfer. The fuel-optimal transfer path is found based on a graph by introducing some simplification. By adding trajectory correction maneuvers, the robust optimal transfer trajectory is achieved in the CR3BP.
AB - The Gateway will be constructed as a staging point for exploring cislunar space in the Artemis program. For the maintenance of this platform, uncrewed cargo transport is planned by JAXA. To efficiently conduct cargo transport, this study proposes a novel methodology to design low-energy chaotic transfers based on lobe dynamics in the planar circular restricted three-body problem (CR3BP). Lobe dynamics focuses on the " lobe, " the region determined by stable and unstable manifolds of a resonant orbit, and can reveal phase space transport of chaotic trajectories. In general, lobe dynamics of one resonant orbit can transfer a spacecraft only around the tori related to the resonant orbit in concern. The proposed method combines lobe dynamics of various resonant orbits to make a desired transfer. The fuel-optimal transfer path is found based on a graph by introducing some simplification. By adding trajectory correction maneuvers, the robust optimal transfer trajectory is achieved in the CR3BP.
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M3 - Conference article
AN - SCOPUS:85187975470
SN - 0074-1795
VL - 2023-October
JO - Proceedings of the International Astronautical Congress, IAC
JF - Proceedings of the International Astronautical Congress, IAC
T2 - 74th International Astronautical Congress, IAC 2023
Y2 - 2 October 2023 through 6 October 2023
ER -