Designing 3D transfers: application to Earth-Moon

arXiv:2609.23496 · astro-ph.EP, astro-ph.IM · Submitted 2026-09-20 · Read on arXiv

astro-ph.EP, astro-ph.IM

Submitted: 2026-09-20

Updated: 2026-09-20

Code: https://github.com/leakec/tfc

License: http://creativecommons.org/licenses/by-nc-nd/4.0/

The gist: Three dimensional Earth-Moon transfers usually consume more fuel than planar ones, but are needed depending on the latitude of the launch site and the desired inclination of the final lunar orbit.

Terminology

Abstract

Three dimensional Earth-Moon transfers usually consume more fuel than planar ones, but are needed depending on the latitude of the launch site and the desired inclination of the final lunar orbit. A systematic search of the optimal 3D transfers represents a true challenge due the dimension of the parameter set to span. In this paper, we propose a new method to design 3D transfers using a tangential velocity constraint for the burns, modeled using the overdetermined constraints technique based on the Theory of Functional Connections for an optimal search of solutions in a numerically efficient way. The developed method is applied here for a systematic study of optimal 3D Earth-Moon transfers, but could be used to design any type of 3D maneuvers.

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