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This paper developes a new method to solve a constant continuous thrust problem via linear purterbuation theory. It speeds up the calculation time significantly, while the accuracy of the solution remains acceptable.
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This page is a summary of: Analytic Approximation for Fixed-Angle Constant Thrust Trajectories via Linear Perturbation Theory, Journal of Guidance Control and Dynamics, January 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g005303.
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