We propose a new method for the detection of energy-efficient trajectories for spacecraft. Via a so called target-shooting approach a pseudo-orbit between the relevant points in space is constructed in a simple model of the problem. This approximate trajectory is meant to serve as input for a more sophisticated direct method in order to compute a true trajectory in the full model. We demonstrate the applicability of the new method by considering the redesign of part of the trajectory of the NASA/JPL Genesis discovery mission.


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    Titel :

    On the Detection of Energetically Efficient Trajectories for Spacecraft


    Beteiligte:
    Dellnitz, Michael (Autor:in) / Junge, Oliver (Autor:in) / Lo, Martin (Autor:in) / Thiere, Bianca (Autor:in)

    Kongress:

    AAS/AIAA Astrodynamics Specialists Conference ; 2001 ; Quebec City, Canada


    Erscheinungsdatum :

    19.07.2001


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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