Calculations are given for Halo satellite orbit control. Previous truncated analytical descriptions were limited and lead to an acceleration error averaging about .000001, which is the 'cost' of a very tight control to the nominal path. The stationkeeping problem is posed so as to permit a looser, optimal three-axis control.


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    Titel :

    Investigation of halo satellite orbit control


    Beteiligte:

    Erscheinungsdatum :

    01.10.1973


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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    Direct lunar halo orbit transfers

    Parker, Jeffrey S. / Born, George H. | Online Contents | 2008