Atmospheric disturbances together with possible deviations in weight and in moment of inertia of vehicle tend to change flight path away from normal flight path; condition for proper cutoff time for rocket power, and proper corrections in elevator angle so that vehicle will land at chosen destination; scheme of tracking and automatic navigation involving high speed computer and elevator servo suggested.


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    Titel :

    Automatic navigation of long range rocket vehicle


    Weitere Titelangaben:

    Am Rocket Soc -- J


    Beteiligte:
    Tsien, H.S. (Autor:in) / Adamson, T.C. (Autor:in) / Knuth, E.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1952


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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