Optimal control theory applied to piecewise constant approximation of large launch booster for first 84 seconds of flight


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    Titel :

    Minimax control of large launch boosters


    Beteiligte:
    Graham, K. D. (Autor:in)

    Erscheinungsdatum :

    1966-07-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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