Advancements in Cislunar Navigation via Modified Orbital Elements

This research addresses a critical need for improved navigation and Space Domain Awareness (SDA) in the cislunar environment. The limitations of conventional Gaussian-based approaches in this region, due to nonlinear dynamics, necessitate the exploration of alternative methodologies. The study's focus on Modified Generalized Equinoctial Orbital Elements, coupled with the Henze-Zirkler test for multivariate normality, represents a significant step towards more accurate uncertainty characterization. The improved preservation of Gaussian behavior demonstrated in the research has direct implications for enhancing the reliability of spacecraft trajectory predictions and collision avoidance strategies. This advancement is particularly relevant in the context of increasing cislunar activity, driven by both governmental and commercial interests. The ability to accurately model and predict spacecraft states is essential for ensuring the safety and sustainability of operations in this increasingly congested region of space. Further research should focus on the computational efficiency and real-time applicability of these methods, as well as their integration with existing SDA infrastructure. The long-term impact of this work could be a more robust and resilient cislunar ecosystem, enabling more ambitious lunar exploration and development initiatives.

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