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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    Title :

    Investigation of halo satellite orbit control


    Contributors:

    Publication date :

    1973-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


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