Analysis reveals differences among SDPT3, SeDuMi, and ECOS solvers, suggesting optimization of fuel consumption.
This article aims to analyze the differences between 3 of the CVX toolbox canonical solvers: SDPT3, SeDuMi and ECOS; for problem formulations based on lossless convexification technique (LCvx). Without loss of generality, the simulations were conducted on the first stage of the launcher Falcon 9, while the goal of the optimization process is to minimize the fuel consumption through minimization of the total thrust under restrictions based on physical limitations of the vehicle.
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BOTEZ et al. (2025) studied this question.
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