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As is well known in celestial mechanics, coordinate choices have significant consequences in the analytical and computational approaches to solve the most fundamental initial value problem. In his work, eight sets of coordinates/elements and their suitability are studied for low-thrust trajectory optimization.

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This page is a summary of: Exploration of Alternative State Vector Choices for Low-Thrust Trajectory Optimization, Journal of Guidance Control and Dynamics, January 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g003686.
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