To model the problem of three bodies in mutual gravitational attaction and present its general solution by Lagrange.

    To develop the restricted three-body problem for modeling the flight of a spacecraft under the gravitational influence of two massive bodies.

    To discuss the solvability, equilibrium points, and numerical solutions of the restricted three-body problem with examples of earth-moon-spacecraft trajectories.


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    Three‐Body Problem

    Cerf, Max | Wiley | 2024


    Three‐Body Problem

    Tewari, Ashish | Wiley | 2021


    The three body problem

    Lemaitre, C. G. | TIBKAT | 1964


    Restricted Three-Body Problem

    Schaub, Hanspeter / Junkins, John L. | AIAA | 2003


    The Restricted Three-Body Problem

    Bonavito, Nino L. / Der, Gim J. / Vinti, John P. | AIAA | 1998