The problem is considered of spacecraft guidance in the stage of distant approach to an orbital station using the second derivative of relative distance as information about rotation of the line of sight.


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    Title :

    Certain Problems of Rendezvous of a Space Vehicle with an Orbital Station


    Contributors:

    Publication date :

    1965


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English