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We analyze the necessary conditions for an optimal landing problem of a rocket in atmosphere. The necessary conditions for the optimality can be either utilized for both validation of solutions found with different methodologies, or implemented to compute optimal trajectories.

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This page is a summary of: Analytical Treatise on Endo-Atmospheric Fuel-Optimal Rocket Landings, Journal of Guidance Control and Dynamics, March 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g008547.
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