Onboard computer equations for rocket vehicle guidance to elliptical orbit, discussing iteration absence from computations and digital simulation results


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    Title :

    A simplified explicit guidance scheme for orbital injection.


    Contributors:

    Conference:

    GUIDANCE, CONTROL AND FLIGHT DYNAMICS CONFERENCE ; 1967 ; HUNTSVILLE, AL


    Publication date :

    1968-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :