Optimization of space-vehicle trajectories by use of iterative guidance mode that minimizes midflight recalculation time for new optimum trajectories


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    Title :

    APPLICATION OF AN ''ITERATIVE GUIDANCE MODE'' TO A LUNAR LANDING


    Contributors:
    Horn, H. J. (author)

    Publication date :

    1963-05-24


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English