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This paper examines the effectiveness of associating space objects in low Earth orbit, focusing on the accuracy of their dynamic models. The authors use mean modified equinoctial elements to minimize the nonlinearity in orbital motion.

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This page is a summary of: Dynamic Model Fidelity Effects on Covariance Based Track Association, Journal of Guidance Control and Dynamics, July 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007871.
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