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In regions where the gravitational attraction of the Earth and Moon are similar in magnitude, the 2-body Keplerian orbital elements are not well-defined. In this work, we develop a local 3-body orbital element analogue.
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This page is a summary of: Local Orbital Elements for the Circular Restricted Three-Body Problem, Journal of Guidance Control and Dynamics, December 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007435.
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