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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    Titel :

    The Three-Body Problem


    Weitere Titelangaben:

    Modeling,Simulation in Science(Birkhäuser)



    Erscheinungsdatum :

    01.01.2007


    Format / Umfang :

    20 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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