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Distant retrograde orbit baseline generation considering solar eclipse mitigation
DOI:10.1016/j.actaastro.2024.06.038.png)
摘要
En 中文
Mitigating solar eclipses presents a formidable challenge in the design of spacecraft orbits, particularly in the case of a distant retrograde orbit (DRO), which is susceptible to significant solar eclipse threats. This paper undertakes a comprehensive analysis of the occurrence characteristics and patterns of both Moon and Earth eclipses on a DRO. The proposed approach involves a two-stage design procedure, encompassing initial orbit selection and orbit extension. The initial orbit selection method primarily focuses on mitigating Earth eclipses by employing the out-of-plane motion inherent in a DRO. The study meticulously explores the influence of three pivotal elements - amplitude, period, and initial phase - on the efficacy of Earth eclipse avoidance. Concurrently, when faced with unavoidable solar eclipses of the initial orbit, a series of tiny maneuvers are systematically applied to extend the baseline orbit. The parameter design space is discretized, and a tree search method is employed to identify viable maneuver sequences. The research successfully achieves the long-term stabilization of the baseline DRO, ensuring that solar eclipses do not exceed 2 h in 10 years. The proposed method's robustness and applicability are substantiated through validation under the ephemeris model.
Keyword:
DRO
Solar eclipse mitigation
Orbit design
Maneuver sequences
期刊
IF:
3.4
论文数:
1.2W
被引数:
2.1W
机构
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