System studied can control aircraft over very large ranges of flight conditions without resort to air data measurements; methods for predicting frequency, amplitude, and effect on performance of inherent limit cycle or "chatter".


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    Title :

    On design of high-gain saturating control system for use as adaptive autopilot


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    48 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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