Orbital Averaging Advancement for Low-Thrust Trajectory Design

被引：0
|
作者：
Astrodynamics & amp [1 ]
Control Systems Group, Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Rd, Laurel
MD
20723, United States
机构：
来源：
J Astronaut Sci | 2024年 / 6卷
关键词：
Geostationary satellites - Orbital transfer - Tropics;
D O I：
10.1007/s40295-024-00468-1
中图分类号：
学科分类号：
摘要：
This work introduces several improvements to the classical orbital averaging approach for the many-revolution low-thrust trajectory problem. The mean anomaly fast variable is included in the averaged state vector to effectively track spacecraft location throughout an orbit transfer. Additionally, a new approach to optimal coasting is formulated based on the relative effectivity concept and is compared to literature results. Both of these improvements are then leveraged to demonstrate a hybrid model that combines averaged and non-averaged dynamics to produce optimal trajectories from Geostationary Transfer Orbit (GTO) to an Earth-Moon Distant Retrograde Orbit (DRO). © The Author(s), under exclusive licence to American Astronautical Society 2024..
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