To investigate the behavior of a spacecraft near a pair of irregular bodies, consider a three body configuration (one massless). Two massive bodies, P.sub.1 and P.sub.2, form the primary system; each primary is initially modeled as an ellipsoid. Concepts and tools similar to those applied in the Circular Restricted Three-Body Problem (CRTBP) are exploited to construct bounded trajectories for a third body in such a synchronous system. Then, to accommodate model uncertainties and other non-gravitational perturbations, a strategy to maintain a spacecraft near a reference path is proposed.


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    Titel :

    Trajectory design for bounded motion near uncertain binary systems comprised of small irregular bodies exploiting sliding control modes


    Beteiligte:

    Erschienen in:

    Acta astronautica ; 115 ; 226-240


    Erscheinungsdatum :

    2015




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :

    Klassifikation :

    BKL:    50.93 / 50.93 Weltraumforschung / 55.60 Raumfahrttechnik / 55.60
    Lokalklassifikation TIB:    050/7040



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