Distant retrograde orbit baseline generation considering solar eclipse mitigation

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...

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Bibliographic Details
Published inActa astronautica Vol. 223; pp. 221 - 233
Main Authors Sun, Yang, Wang, Ming, Zhang, Hao
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.10.2024
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ISSN0094-5765
DOI10.1016/j.actaastro.2024.06.038

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Summary: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. •The occurrence characteristics and patterns of eclipses on DRO are analyzed.•The two-stage design approach contains initial state selection and orbit extension.•The out-of-plane motion of quasi-DRO is leveraged to mitigate Earth eclipses.•Maneuvers are applied to extend the DRO baseline, using the tree search method.•The robustness and applicability of the method validated under the ephemeris model.
ISSN:0094-5765
DOI:10.1016/j.actaastro.2024.06.038