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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    Title :

    Automatic navigation of long range rocket vehicle


    Additional title:

    Am Rocket Soc -- J


    Contributors:
    Tsien, H.S. (author) / Adamson, T.C. (author) / Knuth, E.L. (author)

    Published in:

    Publication date :

    1952


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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