This paper describes new techniques for use in designing possible trajectories to near-Earth objects (NEOs) given the constraints imposed by the limited propulsive capabilities of small satellites and by being launched as a secondary with larger spacecraft. It illustrates the use of these techniques with the design of a trajectory that achieves rendezvous with the NEO 2007 UN12.


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    Titel :

    Trajectory design for small-satellite missions to near-earth objects


    Beteiligte:

    Erscheinungsdatum :

    03.06.2019


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch



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