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This paper presents an exact solution to a fundamental problem in Astrodynamics - The Lambert's problem. All other solution methods are iterative. The main advantages of this new solution method are the high accuracy of the solution and the fast computational speed.
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This page is a summary of: Exact Solution to Lambert’s Problem Using Contour Integrals, Journal of Guidance Control and Dynamics, November 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g008499.
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