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Research ArticleRegular Papers
Open Access

Satellite Ephemeris Parameterization Methods to Support Lunar Positioning, Navigation, and Timing Services

Marta Cortinovis, Keidai Iiyama, and Grace Gao
NAVIGATION: Journal of the Institute of Navigation December 2024, 71 (4) navi.664; DOI: https://doi.org/10.33012/navi.664
Marta Cortinovis
1Department of Aeronautics and Astronautics, Stanford University, California, United States
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Keidai Iiyama,
1Department of Aeronautics and Astronautics, Stanford University, California, United States
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Grace Gao
1Department of Aeronautics and Astronautics, Stanford University, California, United States
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NAVIGATION: Journal of the Institute of Navigation: 71 (4)
NAVIGATION: Journal of the Institute of Navigation
Vol. 71, Issue 4
Winter 2024
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Satellite Ephemeris Parameterization Methods to Support Lunar Positioning, Navigation, and Timing Services
Marta Cortinovis, Keidai Iiyama,, Grace Gao
NAVIGATION: Journal of the Institute of Navigation Dec 2024, 71 (4) navi.664; DOI: 10.33012/navi.664

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Satellite Ephemeris Parameterization Methods to Support Lunar Positioning, Navigation, and Timing Services
Marta Cortinovis, Keidai Iiyama,, Grace Gao
NAVIGATION: Journal of the Institute of Navigation Dec 2024, 71 (4) navi.664; DOI: 10.33012/navi.664
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  • Article
    • Abstract
    • 1 INTRODUCTION
    • 2 LUNAR DYNAMICS AND REFERENCE FRAMES
    • 3 EPHEMERIS PARAMETERIZATION METHODOLOGY
    • 4 EXPERIMENTAL SETUP AND RESULTS
    • 5 CONCLUSIONS
    • HOW TO CITE THIS ARTICLE
    • ACKNOWLEDGMENTS
    • A: USER ALGORITHM FOR STATE DETERMINATION IN THE ME FRAME
    • REFERENCES
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Keywords

  • convex optimization
  • lunar positioning, navigation, and timing
  • satellite ephemeris

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