In this paper, a procedure is described for finding these encounter times using Lambert's theorem and Tisserand's criterion to identify pairs of transfer orbits between the launch planet and intermediate planet and between the intermediate planet and target planet.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Application of Tisserand's criterion to the design of gravity assist trajectories


    Beteiligte:
    Miller, J. K. (Autor:in) / Weeks, C. J. (Autor:in)

    Kongress:

    AIAA Astrodynamics Specialist Conference


    Erscheinungsdatum :

    2002-08-05


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






    AIAA-2002-4717 Application of Tisserand's Criterion to the Design of Gravity Assist Trajectories

    Miller, J. / Weeks, C. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2002


    Rapid Design of Gravity Assist Trajectories

    Carrico, J. / Hooper, H. L. / Roszman, L. et al. | NTRS | 1991