Function of midcourse guidance is to place intercepting vehicle in close proximity to satellite; 2-dimensional geometry and circular target orbits only are considered; equations are developed yielding required velocity corrections necessary for interception as function of rocket's present position and velocity, relative to target; numerical computation.


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    Title :

    Midcourse guidance problem in satellite interception -- 1


    Additional title:

    ARS -- J


    Contributors:

    Published in:

    ARS Journal ; 30 , n 1


    Publication date :

    1960


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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