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.


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    Title :

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


    Contributors:

    Conference:

    AIAA Astrodynamics Specialist Conference


    Publication date :

    2002-08-05


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






    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


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